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Main class for defining the problem; basically this class reads the configuration file, and stores all the information. More...
#include <config_structure.hpp>
Public Member Functions | |
| CConfig (char case_filename[MAX_STRING_SIZE], unsigned short val_software, unsigned short val_iZone, unsigned short val_nZone, unsigned short val_nDim, unsigned short verb_level) | |
| Constructor of the class which reads the input file. More... | |
| CConfig (char case_filename[MAX_STRING_SIZE], unsigned short val_software) | |
| Constructor of the class which reads the input file. More... | |
| CConfig (char case_filename[MAX_STRING_SIZE], CConfig *config) | |
| Constructor of the class which reads the input file. More... | |
| ~CConfig (void) | |
| Destructor of the class. More... | |
| SU2_MPI::Comm | GetMPICommunicator () |
| Get the MPI communicator of SU2. More... | |
| void | SetMPICommunicator (SU2_MPI::Comm Communicator) |
| Set the MPI communicator for SU2. More... | |
| void | SetPointersNull (void) |
| Initializes pointers to null. More... | |
| bool | TokenizeString (string &str, string &option_name, vector< string > &option_value) |
| breaks an input line from the config file into a set of tokens More... | |
| su2double * | GetRefOriginMoment (unsigned short val_marker) |
| Get reference origin for moment computation. More... | |
| su2double | GetRefOriginMoment_X (unsigned short val_marker) |
| Get reference origin x-coordinate for moment computation. More... | |
| su2double | GetRefOriginMoment_Y (unsigned short val_marker) |
| Get reference origin y-coordinate for moment computation. More... | |
| su2double | GetRefOriginMoment_Z (unsigned short val_marker) |
| Get reference origin z-coordinate for moment computation. More... | |
| void | SetRefOriginMoment_X (unsigned short val_marker, su2double val_origin) |
| Set reference origin x-coordinate for moment computation. More... | |
| void | SetRefOriginMoment_Y (unsigned short val_marker, su2double val_origin) |
| Set reference origin y-coordinate for moment computation. More... | |
| void | SetRefOriginMoment_Z (unsigned short val_marker, su2double val_origin) |
| Set reference origin z-coordinate for moment computation. More... | |
| string | GetPlaneTag (unsigned short index) |
| Get index of the upper and lower horizontal plane. More... | |
| su2double | GetEA_IntLimit (unsigned short index) |
| Get the integration limits for the equivalent area computation. More... | |
| su2double | GetEA_ScaleFactor (void) |
| Get the integration limits for the equivalent area computation. More... | |
| su2double | GetAdjointLimit (void) |
| Get the limit value for the adjoint variables. More... | |
| su2double * | GetHold_GridFixed_Coord (void) |
| Get the the coordinates where of the box where the grid is going to be deformed. More... | |
| su2double * | GetSubsonicEngine_Values (void) |
| Get the the coordinates where of the box where a subsonic region is imposed. More... | |
| su2double * | GetSubsonicEngine_Cyl (void) |
| Get the the coordinates where of the box where a subsonic region is imposed. More... | |
| su2double * | GetDistortionRack (void) |
| Get the the coordinates where of the box where a subsonic region is imposed. More... | |
| su2double | GetDualVol_Power (void) |
| Get the power of the dual volume in the grid adaptation sensor. More... | |
| unsigned short | GetAnalytical_Surface (void) |
| Get Information about if there is an analytical definition of the surface for doing the grid adaptation. More... | |
| unsigned short | GetGeo_Description (void) |
| Get Description of the geometry to be analyzed. More... | |
| bool | GetExtraOutput (void) |
| Creates a tecplot file to visualize the partition made by the DDC software. More... | |
| long | GetExtraHeatOutputZone (void) |
| Heat solver zone with extra screen output. More... | |
| su2double | GetMach (void) |
| Get the value of the Mach number (velocity divided by speed of sound). More... | |
| su2double | GetGamma (void) |
| Get the value of the Gamma of fluid (ratio of specific heats). More... | |
| su2double | GetCFL_AdaptParam (unsigned short val_index) |
| Get the values of the CFL adapation. More... | |
| bool | GetCFL_Adapt (void) |
| Get the values of the CFL adapation. More... | |
| su2double | GetHTP_Axis (unsigned short val_index) |
| Get the values of the CFL adapation. More... | |
| su2double | GetStations_Bounds (unsigned short val_var) |
| Get the value of the limits for the sections. More... | |
| su2double | GetFFD_Axis (unsigned short val_var) |
| Get the value of the vector that connects the cartesian axis with a sherical or cylindrical one. More... | |
| su2double | GetBulk_Modulus (void) |
| Get the value of the bulk modulus. More... | |
| su2double | GetBeta_Factor (void) |
| Get the epsilon^2 multiplier for Beta in the incompressible preconditioner. More... | |
| su2double | GetGas_Constant (void) |
| Get the value of specific gas constant. More... | |
| su2double | GetGas_ConstantND (void) |
| Get the value of specific gas constant. More... | |
| su2double | GetMolecular_Weight (void) |
| Get the value of the molecular weight for an incompressible ideal gas (g/mol). More... | |
| su2double | GetSpecific_Heat_Cp (void) |
| Get the value of specific heat at constant pressure. More... | |
| su2double | GetSpecific_Heat_Cp_Solid (void) |
| Get the value of the specific heat for solids. More... | |
| su2double | GetSpecific_Heat_CpND (void) |
| Get the non-dimensional value of specific heat at constant pressure. More... | |
| su2double | GetSpecific_Heat_Cv (void) |
| Get the value of specific heat at constant volume. More... | |
| su2double | GetSpecific_Heat_CvND (void) |
| Get the non-dimensional value of specific heat at constant volume. More... | |
| su2double | GetBlottnerCoeff (unsigned short val_Species, unsigned short val_Coeff) |
| Get the coefficients of the Blottner viscosity model. More... | |
| su2double | GetPnormHeat (void) |
| Get the p-norm for heat-flux objective functions (adjoint problem). More... | |
| su2double | GetWallTemperature (void) |
| Get the value of wall temperature. More... | |
| su2double | GetGas_Constant_Ref (void) |
| Get the reference value for the specific gas constant. More... | |
| su2double | GetHeat_Flux_Ref (void) |
| Get the reference value for the heat flux. More... | |
| su2double | GetTemperature_FreeStream (void) |
| Get the value of the frestream temperature. More... | |
| su2double | GetEnergy_FreeStream (void) |
| Get the value of the frestream temperature. More... | |
| su2double | GetViscosity_FreeStream (void) |
| Get the value of the frestream temperature. More... | |
| su2double | GetDensity_FreeStream (void) |
| Get the value of the frestream temperature. More... | |
| su2double | GetDensity_Solid (void) |
| Get the value of the solid density. More... | |
| su2double | GetModVel_FreeStream (void) |
| Get the value of the frestream temperature. More... | |
| su2double | GetModVel_FreeStreamND (void) |
| Get the value of the frestream temperature. More... | |
| su2double | GetTemperature_ve_FreeStream (void) |
| Get the value of the frestream vibrational-electronic temperature. More... | |
| su2double | GetPrandtl_Lam (void) |
| Get the value of the laminar Prandtl number. More... | |
| su2double | GetPrandtl_Turb (void) |
| Get the value of the turbulent Prandtl number. More... | |
| su2double | GetThermalConductivity_Solid (void) |
| Get the value of the thermal conductivity for solids. More... | |
| su2double | GetThermalDiffusivity_Solid (void) |
| Get the value of the thermal diffusivity for solids. More... | |
| su2double | GetTemperature_Freestream_Solid (void) |
| Get the temperature in solids at freestream conditions. More... | |
| su2double | GetLength_Ref (void) |
| Get the value of the reference length for non-dimensionalization. This value should always be 1 internally, and is not user-specified. More... | |
| su2double | GetPressure_Ref (void) |
| Get the value of the reference pressure for non-dimensionalization. More... | |
| su2double | GetEnergy_Ref (void) |
| Get the value of the reference pressure for non-dimensionalization. More... | |
| su2double | GetTemperature_Ref (void) |
| Get the value of the reference temperature for non-dimensionalization. More... | |
| su2double | GetDensity_Ref (void) |
| Get the value of the reference density for non-dimensionalization. More... | |
| su2double | GetVelocity_Ref (void) |
| Get the value of the reference velocity for non-dimensionalization. More... | |
| su2double | GetTime_Ref (void) |
| Get the value of the reference time for non-dimensionalization. More... | |
| su2double | GetViscosity_Ref (void) |
| Get the value of the reference viscosity for non-dimensionalization. More... | |
| su2double | GetHighlite_Area (void) |
| Get the value of the reference viscosity for non-dimensionalization. More... | |
| su2double | GetFan_Poly_Eff (void) |
| Get the value of the reference viscosity for non-dimensionalization. More... | |
| su2double | GetConductivity_Ref (void) |
| Get the value of the reference conductivity for non-dimensionalization. More... | |
| su2double | GetOmega_Ref (void) |
| Get the value of the reference angular velocity for non-dimensionalization. More... | |
| su2double | GetForce_Ref (void) |
| Get the value of the reference force for non-dimensionalization. More... | |
| su2double | GetPressure_FreeStream (void) |
| Get the value of the non-dimensionalized freestream pressure. More... | |
| su2double | GetPressure_FreeStreamND (void) |
| Get the value of the non-dimensionalized freestream pressure. More... | |
| su2double | GetPressure_Thermodynamic (void) |
| Get the value of the thermodynamic pressure. More... | |
| su2double | GetPressure_ThermodynamicND (void) |
| Get the value of the non-dimensionalized thermodynamic pressure. More... | |
| su2double * | GetVelocity_FreeStream (void) |
| Get the vector of the dimensionalized freestream velocity. More... | |
| su2double | GetTemperature_FreeStreamND (void) |
| Get the value of the non-dimensionalized freestream temperature. More... | |
| su2double | GetDensity_FreeStreamND (void) |
| Get the value of the non-dimensionalized freestream density. More... | |
| su2double * | GetVelocity_FreeStreamND (void) |
| Get the vector of the non-dimensionalized freestream velocity. More... | |
| su2double | GetEnergy_FreeStreamND (void) |
| Get the value of the non-dimensionalized freestream energy. More... | |
| su2double | GetViscosity_FreeStreamND (void) |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetTke_FreeStreamND (void) |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetOmega_FreeStreamND (void) |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetTke_FreeStream (void) |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetOmega_FreeStream (void) |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetIntermittency_FreeStream (void) |
| Get the value of the non-dimensionalized freestream intermittency. More... | |
| su2double | GetTurbulenceIntensity_FreeStream (void) |
| Get the value of the non-dimensionalized freestream turbulence intensity. More... | |
| su2double | GetNuFactor_FreeStream (void) |
| Get the value of the non-dimensionalized freestream turbulence intensity. More... | |
| su2double | GetNuFactor_Engine (void) |
| Get the value of the non-dimensionalized engine turbulence intensity. More... | |
| su2double | GetSecondaryFlow_ActDisk (void) |
| Get the value of the non-dimensionalized actuator disk turbulence intensity. More... | |
| su2double | GetInitial_BCThrust (void) |
| Get the value of the non-dimensionalized actuator disk turbulence intensity. More... | |
| void | SetInitial_BCThrust (su2double val_bcthrust) |
| Get the value of the non-dimensionalized actuator disk turbulence intensity. More... | |
| su2double | GetTurb2LamViscRatio_FreeStream (void) |
| Get the value of the turbulent to laminar viscosity ratio. More... | |
| su2double * | GetMassFrac_FreeStream (void) |
| Get the vector of free stream mass fraction values. More... | |
| su2double | GetLength_Reynolds (void) |
| Get the value of the Reynolds length. More... | |
| unsigned short | GetnStartUpIter (void) |
| Get the start up iterations using the fine grid, this works only for multigrid problems. More... | |
| su2double | GetRefArea (void) |
| Get the reference area for non dimensional coefficient computation. If the value from the is 0 then, the code will compute the reference area using the projection of the shape into the z plane (3D) or the x plane (2D). More... | |
| su2double | GetThermalDiffusivity (void) |
| Get the wave speed. More... | |
| su2double | GetThermal_Expansion_Coeff (void) |
| Get the thermal expansion coefficient. More... | |
| su2double | GetThermal_Expansion_CoeffND (void) |
| Get the non-dim. thermal expansion coefficient. More... | |
| void | SetThermal_Expansion_Coeff (su2double val_thermal_expansion) |
| Set the thermal expansion coefficient. More... | |
| void | SetThermal_Expansion_CoeffND (su2double val_thermal_expansionnd) |
| Set the non-dim. thermal expansion coefficient. More... | |
| su2double | GetInc_Density_Ref (void) |
| Get the value of the reference density for custom incompressible non-dimensionalization. More... | |
| su2double | GetInc_Velocity_Ref (void) |
| Get the value of the reference velocity for custom incompressible non-dimensionalization. More... | |
| su2double | GetInc_Temperature_Ref (void) |
| Get the value of the reference temperature for custom incompressible non-dimensionalization. More... | |
| su2double | GetInc_Density_Init (void) |
| Get the value of the initial density for incompressible flows. More... | |
| su2double * | GetInc_Velocity_Init (void) |
| Get the value of the initial velocity for incompressible flows. More... | |
| su2double | GetInc_Temperature_Init (void) |
| Get the value of the initial temperature for incompressible flows. More... | |
| su2double | GetElasticyMod (unsigned short id_val) |
| Get the Young's modulus of elasticity. More... | |
| bool | GetDE_Effects (void) |
| Decide whether to apply DE effects to the model. More... | |
| bool | GetDE_Predicted (void) |
| Decide whether to predict the DE effects for the next time step. More... | |
| unsigned short | GetnElectric_Constant (void) |
| Get the number of different electric constants. More... | |
| su2double | GetElectric_Constant (unsigned short iVar) |
| Get the value of the DE modulus. More... | |
| su2double | GetKnowles_B (void) |
| Get the value of the B constant in the Knowles material model. More... | |
| su2double | GetKnowles_N (void) |
| Get the value of the N constant in the Knowles material model. More... | |
| unsigned short | GetDV_FEA (void) |
| Get the kind of design variable for FEA. More... | |
| unsigned long | GetRefNode_ID (void) |
| Get the ID of the reference node. More... | |
| su2double | GetRefNode_Displacement (unsigned short val_coeff) |
| Get the values for the reference node displacement. More... | |
| su2double | GetRefNode_Penalty (void) |
| Get the penalty weight value for the objective function. More... | |
| bool | GetRefGeom (void) |
| Decide whether it's necessary to read a reference geometry. More... | |
| string | GetRefGeom_FEMFileName (void) |
| Get the name of the file with the reference geometry of the structural problem. More... | |
| unsigned short | GetRefGeom_FileFormat (void) |
| Get the format of the reference geometry file. More... | |
| unsigned short | GetElas2D_Formulation (void) |
| Formulation for 2D elasticity (plane stress - strain) More... | |
| bool | GetPrestretch (void) |
| Decide whether it's necessary to read a reference geometry. More... | |
| bool | Add_CrossTerm (void) |
| Decide whether it's necessary to add the cross term for adjoint FSI. More... | |
| void | Set_CrossTerm (bool needCrossTerm) |
| Set the boolean addCrossTerm to true or false. More... | |
| string | GetFEA_FileName (void) |
| Get the name of the file with the element properties for structural problems. More... | |
| string | GetPrestretch_FEMFileName (void) |
| Get the name of the file with the reference geometry of the structural problem. More... | |
| su2double | GetPoissonRatio (unsigned short id_val) |
| Get the Poisson's ratio. More... | |
| su2double | GetMaterialDensity (unsigned short id_val) |
| Get the Material Density. More... | |
| unsigned short | GetMaterialCompressibility (void) |
| Compressibility/incompressibility of the solids analysed using the structural solver. More... | |
| unsigned short | GetMaterialModel (void) |
| Compressibility/incompressibility of the solids analysed using the structural solver. More... | |
| unsigned short | GetGeometricConditions (void) |
| Geometric conditions for the structural solver. More... | |
| su2double | GetRefLength (void) |
| Get the reference length for computing moment (the default value is 1). More... | |
| su2double | GetRefElemLength (void) |
| Get the reference element length for computing the slope limiting epsilon. More... | |
| su2double | GetRefSharpEdges (void) |
| Get the reference coefficient for detecting sharp edges. More... | |
| su2double | GetDomainVolume (void) |
| Get the volume of the whole domain using the fine grid, this value is common for all the grids in the multigrid method. More... | |
| void | SetRefArea (su2double val_area) |
| In case the RefArea is equal to 0 then, it is necessary to compute a reference area, with this function we set the value of the reference area. More... | |
| void | SetSemiSpan (su2double val_semispan) |
| In case the SemiSpan is equal to 0 then, it is necessary to compute the max y distance, with this function we set the value of the semi span. More... | |
| void | SetDomainVolume (su2double val_volume) |
| Set the value of the domain volume computed on the finest grid. More... | |
| void | SetFinestMesh (unsigned short val_finestmesh) |
| Set the finest mesh in a multigrid strategy. More... | |
| void | SetKind_TimeIntScheme (unsigned short val_kind_timeintscheme) |
| Set the kind of time integration scheme. More... | |
| void | SetKind_ConvNumScheme (unsigned short val_kind_convnumscheme, unsigned short val_kind_centered, unsigned short val_kind_upwind, unsigned short val_kind_slopelimit, bool val_muscl, unsigned short val_kind_fem) |
| Set the parameters of the convective numerical scheme. More... | |
| su2double | GetVenkat_LimiterCoeff (void) |
| Get the value of limiter coefficient. More... | |
| unsigned long | GetLimiterIter (void) |
| Freeze the value of the limiter after a number of iterations. More... | |
| su2double | GetAdjSharp_LimiterCoeff (void) |
| Get the value of sharp edge limiter. More... | |
| su2double | GetReynolds (void) |
| Get the Reynolds number. Dimensionless number that gives a measure of the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow condition. More... | |
| su2double | GetFroude (void) |
| Get the Froude number for free surface problems. More... | |
| void | SetFroude (su2double val_froude) |
| Set the Froude number for free surface problems. More... | |
| void | SetMach (su2double val_mach) |
| Set the Froude number for free surface problems. More... | |
| void | SetReynolds (su2double val_reynolds) |
| Set the Froude number for free surface problems. More... | |
| void | SetLength_Ref (su2double val_length_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetVelocity_Ref (su2double val_velocity_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetPressure_Ref (su2double val_pressure_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetDensity_Ref (su2double val_density_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetTemperature_Ref (su2double val_temperature_ref) |
| Set the reference temperature. More... | |
| void | SetTime_Ref (su2double val_time_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetEnergy_Ref (su2double val_energy_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetOmega_Ref (su2double val_omega_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetForce_Ref (su2double val_force_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetGas_Constant_Ref (su2double val_gas_constant_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetGas_Constant (su2double val_gas_constant) |
| Set the Froude number for free surface problems. More... | |
| void | SetSpecific_Heat_Cp (su2double val_specific_heat_cp) |
| Set the value of the specific heat at constant pressure (incompressible fluids with energy equation). More... | |
| void | SetSpecific_Heat_CpND (su2double val_specific_heat_cpnd) |
| Set the non-dimensional value of the specific heat at constant pressure (incompressible fluids with energy equation). More... | |
| void | SetSpecific_Heat_Cv (su2double val_specific_heat_cv) |
| Set the value of the specific heat at constant volume (incompressible fluids with energy equation). More... | |
| void | SetSpecific_Heat_CvND (su2double val_specific_heat_cvnd) |
| Set the non-dimensional value of the specific heat at constant volume (incompressible fluids with energy equation). More... | |
| void | SetHeat_Flux_Ref (su2double val_heat_flux_ref) |
| Set the heat flux reference value. More... | |
| void | SetViscosity_Ref (su2double val_viscosity_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetConductivity_Ref (su2double val_conductivity_ref) |
| Set the Froude number for free surface problems. More... | |
| void | SetPressure_FreeStreamND (su2double val_pressure_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetPressure_FreeStream (su2double val_pressure_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetPressure_ThermodynamicND (su2double val_pressure_thermodynamicnd) |
| Set the non-dimensionalized thermodynamic pressure for low Mach problems. More... | |
| void | SetPressure_Thermodynamic (su2double val_pressure_thermodynamic) |
| Set the thermodynamic pressure for low Mach problems. More... | |
| void | SetDensity_FreeStreamND (su2double val_density_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetDensity_FreeStream (su2double val_density_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetViscosity_FreeStream (su2double val_viscosity_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetModVel_FreeStream (su2double val_modvel_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetModVel_FreeStreamND (su2double val_modvel_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetTemperature_FreeStream (su2double val_temperature_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetTemperature_FreeStreamND (su2double val_temperature_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetGas_ConstantND (su2double val_gas_constantnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetVelocity_FreeStream (su2double val_velocity_freestream, unsigned short val_dim) |
| Set the free-stream velocity. More... | |
| void | SetVelocity_FreeStreamND (su2double val_velocity_freestreamnd, unsigned short val_dim) |
| Set the Froude number for free surface problems. More... | |
| void | SetViscosity_FreeStreamND (su2double val_viscosity_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetTke_FreeStreamND (su2double val_tke_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetOmega_FreeStreamND (su2double val_omega_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetTke_FreeStream (su2double val_tke_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetOmega_FreeStream (su2double val_omega_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetEnergy_FreeStreamND (su2double val_energy_freestreamnd) |
| Set the Froude number for free surface problems. More... | |
| void | SetEnergy_FreeStream (su2double val_energy_freestream) |
| Set the Froude number for free surface problems. More... | |
| void | SetThermalDiffusivity_Solid (su2double val_thermal_diffusivity) |
| Set the thermal diffusivity for solids. More... | |
| void | SetTotal_UnstTimeND (su2double val_total_unsttimend) |
| Set the Froude number for free surface problems. More... | |
| su2double | GetAoA (void) |
| Get the angle of attack of the body. This is the angle between a reference line on a lifting body (often the chord line of an airfoil) and the vector representing the relative motion between the lifting body and the fluid through which it is moving. More... | |
| su2double | GetAoA_Offset (void) |
| Get the off set angle of attack of the body. The solution and the geometry file are able to modifity the angle of attack in the config file. More... | |
| su2double | GetAoS_Offset (void) |
| Get the off set sideslip angle of the body. The solution and the geometry file are able to modifity the angle of attack in the config file. More... | |
| su2double | GetAoA_Sens (void) |
| Get the functional sensitivity with respect to changes in the angle of attack. More... | |
| void | SetAoA (su2double val_AoA) |
| Set the angle of attack. More... | |
| void | SetAoA_Offset (su2double val_AoA_offset) |
| Set the off set angle of attack. More... | |
| void | SetAoS_Offset (su2double val_AoS_offset) |
| Set the off set sideslip angle. More... | |
| void | SetAoA_Sens (su2double val_AoA_sens) |
| Set the angle of attack. More... | |
| void | SetAoS (su2double val_AoS) |
| Set the angle of attack. More... | |
| su2double | GetAoS (void) |
| Get the angle of sideslip of the body. It relates to the rotation of the aircraft centerline from the relative wind. More... | |
| su2double | GetChargeCoeff (void) |
| Get the charge coefficient that is used in the poissonal potential simulation. More... | |
| unsigned short | GetnMGLevels (void) |
| Get the number of multigrid levels. More... | |
| void | SetMGLevels (unsigned short val_nMGLevels) |
| Set the number of multigrid levels. More... | |
| unsigned short | GetFinestMesh (void) |
| Get the index of the finest grid. More... | |
| unsigned short | GetMGCycle (void) |
| Get the kind of multigrid (V or W). More... | |
| unsigned short | GetGeometryMode (void) |
| Get the king of evaluation in the geometrical module. More... | |
| su2double | GetCFL (unsigned short val_mesh) |
| Get the Courant Friedrich Levi number for each grid. More... | |
| su2double | GetCFL_Solid (void) |
| Get the Courant Friedrich Levi number for solid solvers. More... | |
| void | SetCFL (unsigned short val_mesh, su2double val_cfl) |
| Get the Courant Friedrich Levi number for each grid. More... | |
| su2double | GetUnst_CFL (void) |
| Get the Courant Friedrich Levi number for unsteady simulations. More... | |
| bool | GetReorientElements (void) |
| Get information about element reorientation. More... | |
| su2double | GetMax_DeltaTime (void) |
| Get the Courant Friedrich Levi number for unsteady simulations. More... | |
| su2double | GetParamDV (unsigned short val_dv, unsigned short val_param) |
| Get a parameter of the particular design variable. More... | |
| su2double | GetCoordFFDBox (unsigned short val_ffd, unsigned short val_index) |
| Get the coordinates of the FFD corner points. More... | |
| unsigned short | GetDegreeFFDBox (unsigned short val_ffd, unsigned short val_index) |
| Get the degree of the FFD corner points. More... | |
| string | GetFFDTag (unsigned short val_dv) |
| Get the FFD Tag of a particular design variable. More... | |
| string | GetTagFFDBox (unsigned short val_ffd) |
| Get the FFD Tag of a particular FFD box. More... | |
| unsigned short | GetnDV (void) |
| Get the number of design variables. More... | |
| unsigned short | GetnDV_Value (unsigned short iDV) |
| Get the number of design variables. More... | |
| unsigned short | GetnFFDBox (void) |
| Get the number of FFD boxes. More... | |
| unsigned short | GetFFD_Continuity (void) |
| Get the required continuity level at the surface intersection with the FFD. More... | |
| unsigned short | GetFFD_CoordSystem (void) |
| Get the coordinate system that we are going to use to define the FFD. More... | |
| unsigned short | GetFFD_Blending (void) |
| Get the kind of FFD Blending function. More... | |
| su2double * | GetFFD_BSplineOrder () |
| Get the kind BSpline Order in i,j,k direction. More... | |
| unsigned short | GetnRKStep (void) |
| Get the number of Runge-Kutta steps. More... | |
| unsigned short | GetnLevels_TimeAccurateLTS (void) |
| Get the number of time levels for time accurate local time stepping. More... | |
| void | SetnLevels_TimeAccurateLTS (unsigned short val_nLevels) |
| Set the number of time levels for time accurate local time stepping. More... | |
| unsigned short | GetnTimeDOFsADER_DG (void) |
| Get the number time DOFs for ADER-DG. More... | |
| su2double * | GetTimeDOFsADER_DG (void) |
| Get the location of the time DOFs for ADER-DG on the interval [-1..1]. More... | |
| unsigned short | GetnTimeIntegrationADER_DG (void) |
| Get the number time integration points for ADER-DG. More... | |
| su2double * | GetTimeIntegrationADER_DG (void) |
| Get the location of the time integration points for ADER-DG on the interval [-1..1]. More... | |
| su2double * | GetWeightsIntegrationADER_DG (void) |
| Get the weights of the time integration points for ADER-DG. More... | |
| unsigned short | GetnMarker_All (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_Max (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_EngineInflow (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_EngineExhaust (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_NearFieldBound (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_InterfaceBound (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_Fluid_InterfaceBound (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_Transpiration (void) |
| Get the total number of transpiration markers. More... | |
| unsigned short | GetnMarker_ActDiskInlet (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_ActDiskOutlet (void) |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_Monitoring (void) |
| Get the total number of monitoring markers. More... | |
| unsigned short | GetnMarker_DV (void) |
| Get the total number of DV markers. More... | |
| unsigned short | GetnMarker_Moving (void) |
| Get the total number of moving markers. More... | |
| unsigned short | GetnMarker_PyCustom (void) |
| Get the total number of Python customizable markers. More... | |
| unsigned short | GetnMarker_Analyze (void) |
| Get the total number of moving markers. More... | |
| unsigned short | GetnMarker_Periodic (void) |
| Get the total number of periodic markers. More... | |
| unsigned short | GetnMarker_HeatFlux (void) |
| Get the total number of heat flux markers. More... | |
| unsigned short | GetnObj (void) |
| Get the total number of objectives in kind_objective list. More... | |
| void | SetnMarker_All (unsigned short val_nmarker) |
| Stores the number of marker in the simulation. More... | |
| unsigned long | GetnExtIter (void) |
| Get the number of external iterations. More... | |
| unsigned long | GetUnst_nIntIter (void) |
| Get the number of internal iterations. More... | |
| unsigned long | GetDyn_nIntIter (void) |
| Get the number of internal iterations for the Newton-Raphson Method in nonlinear structural applications. More... | |
| long | GetUnst_RestartIter (void) |
| Get the restart iteration number for unsteady simulations. More... | |
| long | GetUnst_AdjointIter (void) |
| Get the starting direct iteration number for the unsteady adjoint (reverse time integration). More... | |
| unsigned long | GetIter_Avg_Objective (void) |
| Number of iterations to average (reverse time integration). More... | |
| long | GetDyn_RestartIter (void) |
| Get the restart iteration number for dynamic structural simulations. More... | |
| unsigned short | GetnTimeInstances (void) |
| Retrieves the number of periodic time instances for Harmonic Balance. More... | |
| su2double | GetHarmonicBalance_Period (void) |
| Retrieves the period of oscillations to be used with Harmonic Balance. More... | |
| void | SetnExtIter (unsigned long val_niter) |
| Set the number of external iterations. More... | |
| void | SetExtIter (unsigned long val_iter) |
| Set the current external iteration number. More... | |
| void | SetExtIter_OffSet (unsigned long val_iter) |
| Set the current external iteration number. More... | |
| void | SetFSIIter (unsigned long val_iter) |
| Set the current FSI iteration number. More... | |
| void | SetIntIter (unsigned long val_iter) |
| Set the current internal iteration number. More... | |
| unsigned long | GetExtIter (void) |
| Get the current external iteration number. More... | |
| unsigned long | GetExtIter_OffSet (void) |
| Get the current internal iteration number. More... | |
| unsigned long | GetFSIIter (void) |
| Get the current FSI iteration number. More... | |
| unsigned long | GetIntIter (void) |
| Get the current internal iteration number. More... | |
| unsigned long | GetWrt_Sol_Freq (void) |
| Get the frequency for writing the solution file. More... | |
| unsigned long | GetWrt_Sol_Freq_DualTime (void) |
| Get the frequency for writing the solution file in Dual Time. More... | |
| unsigned long | GetWrt_Con_Freq (void) |
| Get the frequency for writing the convergence file. More... | |
| void | SetWrt_Con_Freq (unsigned long val_freq) |
| Set the frequency for writing the convergence file. More... | |
| unsigned long | GetWrt_Con_Freq_DualTime (void) |
| Get the frequency for writing the convergence file in Dual Time. More... | |
| bool | GetWrt_Unsteady (void) |
| Get information about writing unsteady headers and file extensions. More... | |
| bool | GetWrt_Output (void) |
| Get information about writing output files. More... | |
| bool | GetWrt_Vol_Sol (void) |
| Get information about writing a volume solution file. More... | |
| bool | GetLow_MemoryOutput (void) |
| Get information about writing a volume solution file. More... | |
| bool | GetWrt_Srf_Sol (void) |
| Get information about writing a surface solution file. More... | |
| bool | GetWrt_Csv_Sol (void) |
| Get information about writing a surface comma-separated values (CSV) solution file. More... | |
| bool | GetWrt_Crd_Sol (void) |
| Get information about writing a binary coordinates file. More... | |
| bool | GetWrt_Residuals (void) |
| Get information about writing residuals to volume solution file. More... | |
| bool | GetWrt_Limiters (void) |
| Get information about writing residuals to volume solution file. More... | |
| bool | GetWrt_Surface (void) |
| Write solution at each surface. More... | |
| bool | GetWrt_SharpEdges (void) |
| Get information about writing residuals to volume solution file. More... | |
| bool | GetWrt_Halo (void) |
| Get information about writing rind layers to the solution files. More... | |
| bool | GetWrt_Performance (void) |
| Get information about writing the performance summary at the end of a calculation. More... | |
| bool | GetWrt_InletFile (void) |
| Get information about writing a template inlet profile file. More... | |
| void | SetWrt_InletFile (bool val_wrt_inletfile) |
| Set information about writing a template inlet profile file. More... | |
| bool | GetWrt_Slice (void) |
| Get information about writing a 1D slice of a 2D cartesian solution. More... | |
| bool | GetPlot_Section_Forces (void) |
| Get information about writing sectional force files. More... | |
| su2double | Get_Alpha_RKStep (unsigned short val_step) |
| Get the alpha (convective) coefficients for the Runge-Kutta integration scheme. More... | |
| string | GetMarker_All_TagBound (unsigned short val_marker) |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_ActDiskInlet_TagBound (unsigned short val_marker) |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_ActDiskOutlet_TagBound (unsigned short val_marker) |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_EngineInflow_TagBound (unsigned short val_marker) |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_EngineExhaust_TagBound (unsigned short val_marker) |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_Monitoring_TagBound (unsigned short val_marker) |
| Get the name of the surface defined in the geometry file. More... | |
| string | GetMarker_HeatFlux_TagBound (unsigned short val_marker) |
| Get the name of the surface defined in the geometry file. More... | |
| short | GetMarker_All_TagBound (string val_tag) |
| Get the tag if the iMarker defined in the geometry file. More... | |
| unsigned short | GetMarker_All_KindBC (unsigned short val_marker) |
| Get the kind of boundary for each marker. More... | |
| void | SetMarker_All_KindBC (unsigned short val_marker, unsigned short val_boundary) |
| Set the value of the boundary val_boundary (read from the config file) for the marker val_marker. More... | |
| void | SetMarker_All_TagBound (unsigned short val_marker, string val_index) |
| Set the value of the index val_index (read from the geometry file) for the marker val_marker. More... | |
| void | SetMarker_All_Monitoring (unsigned short val_marker, unsigned short val_monitoring) |
| Set if a marker val_marker is going to be monitored val_monitoring (read from the config file). More... | |
| void | SetMarker_All_GeoEval (unsigned short val_marker, unsigned short val_geoeval) |
| Set if a marker val_marker is going to be monitored val_monitoring (read from the config file). More... | |
| void | SetMarker_All_Designing (unsigned short val_marker, unsigned short val_designing) |
| Set if a marker val_marker is going to be designed val_designing (read from the config file). More... | |
| void | SetMarker_All_Plotting (unsigned short val_marker, unsigned short val_plotting) |
| Set if a marker val_marker is going to be plot val_plotting (read from the config file). More... | |
| void | SetMarker_All_Analyze (unsigned short val_marker, unsigned short val_analyze) |
| Set if a marker val_marker is going to be plot val_plotting (read from the config file). More... | |
| void | SetMarker_All_ZoneInterface (unsigned short val_marker, unsigned short val_fsiinterface) |
| Set if a marker val_marker is part of the FSI interface val_plotting (read from the config file). More... | |
| void | SetMarker_All_Turbomachinery (unsigned short val_marker, unsigned short val_turbo) |
| Set if a marker val_marker is part of the Turbomachinery (read from the config file). More... | |
| void | SetMarker_All_TurbomachineryFlag (unsigned short val_marker, unsigned short val_turboflag) |
| Set a flag to the marker val_marker part of the Turbomachinery (read from the config file). More... | |
| void | SetMarker_All_MixingPlaneInterface (unsigned short val_marker, unsigned short val_mixplan_interface) |
| Set if a marker val_marker is part of the MixingPlane interface (read from the config file). More... | |
| void | SetMarker_All_DV (unsigned short val_marker, unsigned short val_DV) |
| Set if a marker val_marker is going to be affected by design variables val_moving (read from the config file). More... | |
| void | SetMarker_All_Moving (unsigned short val_marker, unsigned short val_moving) |
| Set if a marker val_marker is going to be moved val_moving (read from the config file). More... | |
| void | SetMarker_All_PyCustom (unsigned short val_marker, unsigned short val_PyCustom) |
| Set if a marker val_marker is going to be customized in Python val_PyCustom (read from the config file). More... | |
| void | SetMarker_All_PerBound (unsigned short val_marker, short val_perbound) |
| Set if a marker val_marker is going to be periodic val_perbound (read from the config file). More... | |
| void | SetMarker_All_SendRecv (unsigned short val_marker, short val_index) |
| Set if a marker val_marker is going to be sent or receive val_index from another domain. More... | |
| short | GetMarker_All_SendRecv (unsigned short val_marker) |
| Get the send-receive information for a marker val_marker. More... | |
| short | GetMarker_All_PerBound (unsigned short val_marker) |
| Get an internal index that identify the periodic boundary conditions. More... | |
| unsigned short | GetMarker_All_Monitoring (unsigned short val_marker) |
| Get the monitoring information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_GeoEval (unsigned short val_marker) |
| Get the monitoring information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Designing (unsigned short val_marker) |
| Get the design information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Plotting (unsigned short val_marker) |
| Get the plotting information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Analyze (unsigned short val_marker) |
| Get the plotting information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_ZoneInterface (unsigned short val_marker) |
| Get the FSI interface information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_MixingPlaneInterface (unsigned short val_marker) |
| Get the MixingPlane interface information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Turbomachinery (unsigned short val_marker) |
| Get the Turbomachinery information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_TurbomachineryFlag (unsigned short val_marker) |
| Get the Turbomachinery flag information for a marker val_marker. More... | |
| unsigned short | GetMarker_n_ZoneInterface (void) |
| Get the number of FSI interface markers val_marker. More... | |
| unsigned short | GetMarker_All_DV (unsigned short val_marker) |
| Get the DV information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Moving (unsigned short val_marker) |
| Get the motion information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_PyCustom (unsigned short val_marker) |
| Get the Python customization for a marker val_marker. More... | |
| su2double | GetLocationStations (unsigned short val_section) |
| Get the airfoil sections in the slicing process. More... | |
| su2double | GetNacelleLocation (unsigned short val_index) |
| Get the defintion of the nacelle location. More... | |
| unsigned short | GetMG_PreSmooth (unsigned short val_mesh) |
| Get the number of pre-smoothings in a multigrid strategy. More... | |
| unsigned short | GetMG_PostSmooth (unsigned short val_mesh) |
| Get the number of post-smoothings in a multigrid strategy. More... | |
| unsigned short | GetMG_CorrecSmooth (unsigned short val_mesh) |
| Get the number of implicit Jacobi smoothings of the correction in a multigrid strategy. More... | |
| short | GetFFD_Fix_IDir (unsigned short val_index) |
| plane of the FFD (I axis) that should be fixed. More... | |
| short | GetFFD_Fix_JDir (unsigned short val_index) |
| plane of the FFD (J axis) that should be fixed. More... | |
| short | GetFFD_Fix_KDir (unsigned short val_index) |
| plane of the FFD (K axis) that should be fixed. More... | |
| unsigned short | GetnFFD_Fix_IDir (void) |
| Get the number of planes to fix in the I direction. More... | |
| unsigned short | GetnFFD_Fix_JDir (void) |
| Get the number of planes to fix in the J direction. More... | |
| unsigned short | GetnFFD_Fix_KDir (void) |
| Get the number of planes to fix in the K direction. More... | |
| unsigned short | GetKind_Solver (void) |
| Governing equations of the flow (it can be different from the run time equation). More... | |
| void | SetKind_Solver (unsigned short val_solver) |
| Governing equations of the flow (it can be different from the run time equation). More... | |
| unsigned short | GetKind_Regime (void) |
| Governing equations of the flow (it can be different from the run time equation). More... | |
| unsigned short | GetSystemMeasurements (void) |
| Governing equations of the flow (it can be different from the run time equation). More... | |
| unsigned short | GetKind_GasModel (void) |
| Gas model that we are using. More... | |
| unsigned short | GetKind_FluidModel (void) |
| Fluid model that we are using. More... | |
| unsigned short | GetKind_DensityModel (void) |
| Option to define the density model for incompressible flows. More... | |
| bool | GetEnergy_Equation (void) |
| Flag for whether to solve the energy equation for incompressible flows. More... | |
| unsigned short | GetKind_FreeStreamOption (void) |
| free stream option to initialize the solution More... | |
| unsigned short | GetKind_InitOption (void) |
| free stream option to initialize the solution More... | |
| su2double | GetPressure_Critical (void) |
| Get the value of the critical pressure. More... | |
| su2double | GetTemperature_Critical (void) |
| Get the value of the critical temperature. More... | |
| su2double | GetAcentric_Factor (void) |
| Get the value of the critical pressure. More... | |
| unsigned short | GetKind_ViscosityModel (void) |
| Get the value of the viscosity model. More... | |
| unsigned short | GetKind_ConductivityModel (void) |
| Get the value of the thermal conductivity model. More... | |
| su2double | GetMu_Constant (void) |
| Get the value of the constant viscosity. More... | |
| su2double | GetMu_ConstantND (void) |
| Get the value of the non-dimensional constant viscosity. More... | |
| su2double | GetKt_Constant (void) |
| Get the value of the thermal conductivity. More... | |
| su2double | GetKt_ConstantND (void) |
| Get the value of the non-dimensional thermal conductivity. More... | |
| su2double | GetMu_Ref (void) |
| Get the value of the reference viscosity for Sutherland model. More... | |
| su2double | GetMu_RefND (void) |
| Get the value of the non-dimensional reference viscosity for Sutherland model. More... | |
| su2double | GetMu_Temperature_Ref (void) |
| Get the value of the reference temperature for Sutherland model. More... | |
| su2double | GetMu_Temperature_RefND (void) |
| Get the value of the non-dimensional reference temperature for Sutherland model. More... | |
| su2double | GetMu_S (void) |
| Get the value of the reference S for Sutherland model. More... | |
| su2double | GetMu_SND (void) |
| Get the value of the non-dimensional reference S for Sutherland model. More... | |
| void | SetMu_ConstantND (su2double mu_const) |
| Set the value of the non-dimensional constant viscosity. More... | |
| void | SetKt_ConstantND (su2double kt_const) |
| Set the value of the non-dimensional thermal conductivity. More... | |
| void | SetMu_RefND (su2double mu_ref) |
| Set the value of the non-dimensional reference viscosity for Sutherland model. More... | |
| void | SetMu_Temperature_RefND (su2double mu_Tref) |
| Set the value of the non-dimensional reference temperature for Sutherland model. More... | |
| void | SetMu_SND (su2double mu_s) |
| Set the value of the non-dimensional S for Sutherland model. More... | |
| unsigned short | GetKind_Gradient_Method (void) |
| Get the kind of method for computation of spatial gradients. More... | |
| unsigned short | GetKind_Linear_Solver (void) |
| Get the kind of solver for the implicit solver. More... | |
| unsigned short | GetKind_Linear_Solver_Prec (void) |
| Get the kind of preconditioner for the implicit solver. More... | |
| unsigned short | GetKind_Deform_Linear_Solver (void) |
| Get the kind of solver for the implicit solver. More... | |
| void | SetKind_Deform_Linear_Solver_Prec (unsigned short val_kind_prec) |
| Set the kind of preconditioner for the implicit solver. More... | |
| void | SetKind_Linear_Solver_Prec (unsigned short val_kind_prec) |
| Set the kind of preconditioner for the implicit solver. More... | |
| su2double | GetLinear_Solver_Error (void) |
| Get min error of the linear solver for the implicit formulation. More... | |
| su2double | GetDeform_Linear_Solver_Error (void) |
| Get min error of the linear solver for the implicit formulation. More... | |
| unsigned long | GetLinear_Solver_Iter (void) |
| Get max number of iterations of the linear solver for the implicit formulation. More... | |
| unsigned long | GetDeform_Linear_Solver_Iter (void) |
| Get max number of iterations of the linear solver for the implicit formulation. More... | |
| unsigned short | GetLinear_Solver_ILU_n (void) |
| Get the ILU fill-in level for the linear solver. More... | |
| unsigned long | GetLinear_Solver_Restart_Frequency (void) |
| Get restart frequency of the linear solver for the implicit formulation. More... | |
| su2double | GetRelaxation_Factor_Flow (void) |
| Get the relaxation coefficient of the linear solver for the implicit formulation. More... | |
| su2double | GetRelaxation_Factor_AdjFlow (void) |
| Get the relaxation coefficient of the linear solver for the implicit formulation. More... | |
| su2double | GetRelaxation_Factor_Turb (void) |
| Get the relaxation coefficient of the linear solver for the implicit formulation. More... | |
| su2double | GetRelaxation_Factor_CHT (void) |
| Get the relaxation coefficient of the CHT coupling. More... | |
| su2double | GetRoe_Kappa (void) |
| Get the relaxation coefficient of the linear solver for the implicit formulation. More... | |
| su2double | GetSemiSpan (void) |
| Get the wing semi span. More... | |
| unsigned short | GetKind_AdjTurb_Linear_Solver (void) |
| Get the kind of solver for the implicit solver. More... | |
| unsigned short | GetKind_AdjTurb_Linear_Prec (void) |
| Get the kind of preconditioner for the implicit solver. More... | |
| unsigned short | GetKind_DiscAdj_Linear_Solver (void) |
| Get the kind of solver for the implicit solver. More... | |
| unsigned short | GetKind_DiscAdj_Linear_Prec (void) |
| Get the kind of preconditioner for the implicit solver. More... | |
| unsigned short | GetKind_Deform_Linear_Solver_Prec (void) |
| Get the kind of preconditioner for the implicit solver. More... | |
| void | SetKind_AdjTurb_Linear_Prec (unsigned short val_kind_prec) |
| Set the kind of preconditioner for the implicit solver. More... | |
| su2double | GetAdjTurb_Linear_Error (void) |
| Get min error of the linear solver for the implicit formulation. More... | |
| su2double | GetEntropyFix_Coeff (void) |
| Get the entropy fix. More... | |
| unsigned short | GetAdjTurb_Linear_Iter (void) |
| Get max number of iterations of the linear solver for the implicit formulation. More... | |
| su2double | GetCFLRedCoeff_AdjTurb (void) |
| Get CFL reduction factor for adjoint turbulence model. More... | |
| unsigned long | GetGridDef_Linear_Iter (void) |
| Get the number of linear smoothing iterations for mesh deformation. More... | |
| unsigned long | GetGridDef_Nonlinear_Iter (void) |
| Get the number of nonlinear increments for mesh deformation. More... | |
| bool | GetDeform_Output (void) |
| Get information about writing grid deformation residuals to the console. More... | |
| su2double | GetDeform_Tol_Factor (void) |
| Get factor to multiply smallest volume for deform tolerance. More... | |
| su2double | GetDeform_Coeff (void) |
| Get factor to multiply smallest volume for deform tolerance. More... | |
| su2double | GetDeform_Limit (void) |
| Get limit for the volumetric deformation. More... | |
| su2double | GetDeform_ElasticityMod (void) |
| Get Young's modulus for deformation (constant stiffness deformation) More... | |
| su2double | GetDeform_PoissonRatio (void) |
| Get Poisson's ratio for deformation (constant stiffness deformation) . More... | |
| unsigned short | GetDeform_Stiffness_Type (void) |
| Get the type of stiffness to impose for FEA mesh deformation. More... | |
| bool | GetVisualize_Volume_Def (void) |
| Creates a tecplot file to visualize the volume deformation deformation made by the DEF software. More... | |
| bool | GetVisualize_Surface_Def (void) |
| Creates a teot file to visualize the surface deformation deformation made by the DEF software. More... | |
| bool | GetFFD_Symmetry_Plane (void) |
| Define the FFD box with a symetry plane. More... | |
| unsigned short | GetKind_SU2 (void) |
| Get the kind of SU2 software component. More... | |
| unsigned short | GetRef_NonDim (void) |
| Get the kind of non-dimensionalization. More... | |
| unsigned short | GetRef_Inc_NonDim (void) |
| Get the kind of incompressible non-dimensionalization. More... | |
| void | SetKind_SU2 (unsigned short val_kind_su2) |
| Get the kind of SU2 software component. More... | |
| unsigned short | GetKind_Turb_Model (void) |
| Get the kind of the turbulence model. More... | |
| unsigned short | GetKind_Trans_Model (void) |
| Get the kind of the transition model. More... | |
| unsigned short | GetKind_SGS_Model (void) |
| Get the kind of the subgrid scale model. More... | |
| unsigned short | GetKind_Adaptation (void) |
| Get the kind of adaptation technique. More... | |
| su2double | GetNew_Elem_Adapt (void) |
| Get the number of new elements added in the adaptation process. More... | |
| unsigned short | GetKind_TimeIntScheme (void) |
| Get the kind of time integration method. More... | |
| unsigned short | GetKind_ConvNumScheme (void) |
| Get the kind of convective numerical scheme. More... | |
| unsigned short | GetKind_Centered (void) |
| Get kind of center scheme for the convective terms. More... | |
| unsigned short | GetKind_Upwind (void) |
| Get kind of upwind scheme for the convective terms. More... | |
| bool | GetMUSCL (void) |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_Flow (void) |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_Heat (void) |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_Turb (void) |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_AdjFlow (void) |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_AdjTurb (void) |
| Get if the upwind scheme used MUSCL or not. More... | |
| unsigned short | GetKind_TimeIntScheme_Flow (void) |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_ADER_Predictor (void) |
| Get the kind of scheme (aliased or non-aliased) to be used in the predictor step of ADER-DG. More... | |
| unsigned short | GetKind_TimeIntScheme_Heat (void) |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_TimeStep_Heat (void) |
| Get the kind of time stepping for the heat equation. More... | |
| unsigned short | GetKind_TimeIntScheme_FEA (void) |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_TimeIntScheme_Template (void) |
| Get the kind of integration scheme (explicit or implicit) for the template equations. More... | |
| unsigned short | GetKind_SpaceIteScheme_FEA (void) |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_TransferMethod (void) |
| Get the kind of transfer method we want to use for multiphysics problems. More... | |
| unsigned short | GetKind_ConvNumScheme_Flow (void) |
| Get the kind of convective numerical scheme for the flow equations (centered or upwind). More... | |
| unsigned short | GetKind_ConvNumScheme_FEM_Flow (void) |
| Get the kind of convective numerical scheme for the flow equations (finite element). More... | |
| unsigned short | GetKind_ConvNumScheme_Template (void) |
| Get the kind of convective numerical scheme for the template equations (centered or upwind). More... | |
| unsigned short | GetKind_Centered_Flow (void) |
| Get the kind of center convective numerical scheme for the flow equations. More... | |
| unsigned short | GetKind_Centered_Template (void) |
| Get the kind of center convective numerical scheme for the plasma equations. More... | |
| unsigned short | GetKind_Upwind_Flow (void) |
| Get the kind of upwind convective numerical scheme for the flow equations. More... | |
| unsigned short | GetKind_FEM_Flow (void) |
| Get the kind of finite element convective numerical scheme for the flow equations. More... | |
| unsigned short | GetKind_FEM_DG_Shock (void) |
| Get the kind of shock capturing method in FEM DG solver. More... | |
| unsigned short | GetKind_Matrix_Coloring (void) |
| Get the kind of matrix coloring used for the sparse Jacobian computation. More... | |
| unsigned short | GetKind_SlopeLimit (void) |
| Get the method for limiting the spatial gradients. More... | |
| unsigned short | GetKind_SlopeLimit_Flow (void) |
| Get the method for limiting the spatial gradients. More... | |
| unsigned short | GetKind_SlopeLimit_Turb (void) |
| Get the method for limiting the spatial gradients. More... | |
| unsigned short | GetKind_SlopeLimit_AdjTurb (void) |
| Get the method for limiting the spatial gradients. More... | |
| unsigned short | GetKind_SlopeLimit_AdjFlow (void) |
| Get the method for limiting the spatial gradients. More... | |
| su2double | GetKappa_1st_Flow (void) |
| Value of the calibrated constant for the Lax method (center scheme). More... | |
| su2double | GetKappa_2nd_Flow (void) |
| Value of the calibrated constant for the JST method (center scheme). More... | |
| su2double | GetKappa_4th_Flow (void) |
| Value of the calibrated constant for the JST method (center scheme). More... | |
| su2double | GetKappa_2nd_Heat (void) |
| Value of the calibrated constant for the JST method (center scheme). More... | |
| su2double | GetKappa_4th_Heat (void) |
| Value of the calibrated constant for the JST-like method (center scheme). More... | |
| unsigned short | GetKind_TimeIntScheme_AdjFlow (void) |
| Get the kind of integration scheme (explicit or implicit) for the adjoint flow equations. More... | |
| unsigned short | GetKind_ConvNumScheme_AdjFlow (void) |
| Get the kind of convective numerical scheme for the adjoint flow equations (centered or upwind). More... | |
| unsigned short | GetKind_Centered_AdjFlow (void) |
| Get the kind of center convective numerical scheme for the adjoint flow equations. More... | |
| unsigned short | GetKind_Upwind_AdjFlow (void) |
| Get the kind of upwind convective numerical scheme for the adjoint flow equations. More... | |
| su2double | GetKappa_2nd_AdjFlow (void) |
| Value of the calibrated constant for the high order method (center scheme). More... | |
| su2double | GetKappa_4th_AdjFlow (void) |
| Value of the calibrated constant for the high order method (center scheme). More... | |
| su2double | GetKappa_1st_AdjFlow (void) |
| Value of the calibrated constant for the low order method (center scheme). More... | |
| unsigned short | GetKind_TimeIntScheme_Turb (void) |
| Get the kind of integration scheme (implicit) for the turbulence equations. More... | |
| unsigned short | GetKind_ConvNumScheme_Turb (void) |
| Get the kind of convective numerical scheme for the turbulence equations (upwind). More... | |
| unsigned short | GetKind_Centered_Turb (void) |
| Get the kind of center convective numerical scheme for the turbulence equations. More... | |
| unsigned short | GetKind_Upwind_Turb (void) |
| Get the kind of upwind convective numerical scheme for the turbulence equations. More... | |
| unsigned short | GetKind_TimeIntScheme_AdjTurb (void) |
| Get the kind of integration scheme (explicit or implicit) for the adjoint turbulence equations. More... | |
| unsigned short | GetKind_ConvNumScheme_AdjTurb (void) |
| Get the kind of convective numerical scheme for the adjoint turbulence equations (centered or upwind). More... | |
| unsigned short | GetKind_ConvNumScheme_Heat (void) |
| Get the kind of convective numerical scheme for the heat equation. More... | |
| unsigned short | GetKind_Centered_AdjTurb (void) |
| Get the kind of center convective numerical scheme for the adjoint turbulence equations. More... | |
| unsigned short | GetKind_Upwind_AdjTurb (void) |
| Get the kind of upwind convective numerical scheme for the adjoint turbulence equations. More... | |
| bool | GetFrozen_Visc_Cont (void) |
| Provides information about the way in which the turbulence will be treated by the cont. adjoint method. More... | |
| bool | GetFrozen_Visc_Disc (void) |
| Provides information about the way in which the turbulence will be treated by the disc. adjoint method. More... | |
| bool | GetInconsistent_Disc (void) |
| Provides information about using an inconsistent (primal/dual) discrete adjoint formulation. More... | |
| bool | GetFrozen_Limiter_Disc (void) |
| Provides information about the way in which the limiter will be treated by the disc. adjoint method. More... | |
| bool | GetWrite_Conv_FSI (void) |
| Write convergence file for FSI problems. More... | |
| bool | GetSens_Remove_Sharp (void) |
| Provides information about if the sharp edges are going to be removed from the sensitivity. More... | |
| unsigned short | GetKind_Inlet (void) |
| Get the kind of inlet boundary condition treatment (total conditions or mass flow). More... | |
| bool | GetInlet_Profile_From_File (void) |
| Check if the inlet profile(s) are specified in an input file. More... | |
| string | GetInlet_FileName (void) |
| Get name of the input file for the specified inlet profile. More... | |
| su2double | GetInlet_Profile_Matching_Tolerance (void) |
| Get the tolerance used for matching two points on a specified inlet. More... | |
| unsigned short | GetKind_Inc_Inlet (string val_marker) |
| Get the type of incompressible inlet from the list. More... | |
| unsigned short | GetnInc_Inlet (void) |
| Get the total number of types in Kind_Inc_Inlet list. More... | |
| bool | GetInc_Inlet_UseNormal (void) |
| Flag for whether the local boundary normal is used as the flow direction for an incompressible pressure inlet. More... | |
| unsigned short | GetKind_AverageProcess (void) |
| Get the kind of mixing process for averaging quantities at the boundaries. More... | |
| unsigned short | GetKind_PerformanceAverageProcess (void) |
| Get the kind of mixing process for averaging quantities at the boundaries. More... | |
| void | SetKind_AverageProcess (unsigned short new_AverageProcess) |
| Set the kind of mixing process for averaging quantities at the boundaries. More... | |
| void | SetKind_PerformanceAverageProcess (unsigned short new_AverageProcess) |
| Set the kind of mixing process for averaging quantities at the boundaries. More... | |
| su2double | GetRampRotatingFrame_Coeff (unsigned short iCoeff) |
| Get coeff for Rotating Frame Ramp. More... | |
| bool | GetRampRotatingFrame (void) |
| Get Rotating Frame Ramp option. More... | |
| su2double | GetRampOutletPressure_Coeff (unsigned short iCoeff) |
| Get coeff for Outlet Pressure Ramp. More... | |
| su2double | GetFinalOutletPressure (void) |
| Get final Outlet Pressure value for the ramp. More... | |
| su2double | GetMonitorOutletPressure (void) |
| Get final Outlet Pressure value for the ramp. More... | |
| void | SetMonitotOutletPressure (su2double newMonPres) |
| Set Monitor Outlet Pressure value for the ramp. More... | |
| bool | GetRampOutletPressure (void) |
| Get Outlet Pressure Ramp option. More... | |
| su2double | GetMixedout_Coeff (unsigned short iCoeff) |
| Get mixedout coefficients. More... | |
| su2double | GetExtraRelFacGiles (unsigned short iCoeff) |
| Get extra relaxation factor coefficients for the Giels BC. More... | |
| su2double | GetAverageMachLimit (void) |
| Get mach limit for average massflow-based procedure . More... | |
| unsigned short | GetKind_MixingPlaneInterface (void) |
| Get the kind of mixing process for averaging quantities at the boundaries. More... | |
| unsigned short | GetKind_TurboMachinery (unsigned short val_iZone) |
| Get the kind of turbomachinery architecture. More... | |
| unsigned short | GetKind_SpanWise (void) |
| Get the kind of turbomachinery architecture. More... | |
| bool | GetBoolMixingPlaneInterface (void) |
| Verify if there is mixing plane interface specified from config file. More... | |
| bool | GetBoolTurbMixingPlane (void) |
| Verify if there is mixing plane interface specified from config file. More... | |
| bool | GetSpatialFourier (void) |
| Verify if there is mixing plane interface specified from config file. More... | |
| unsigned short | GetnMarker_MixingPlaneInterface (void) |
| number mixing plane interface specified from config file. More... | |
| bool | GetBoolTurbomachinery (void) |
| Verify if there is Turbomachinery performance option specified from config file. More... | |
| bool | GetBoolZoneSpecific (void) |
| Verify if there are zone specific solvers entered in the config file. More... | |
| su2double | GetnBlades (unsigned short val_iZone) |
| number Turbomachinery blades computed using the pitch information. More... | |
| void | SetnBlades (unsigned short val_iZone, su2double nblades) |
| number Turbomachinery blades computed using the pitch information. More... | |
| bool | GetBoolGiles (void) |
| Verify if there is any Giles Boundary Condition option specified from config file. More... | |
| bool | GetBoolRiemann (void) |
| Verify if there is any Riemann Boundary Condition option specified from config file. More... | |
| unsigned short | GetnMarker_Turbomachinery (void) |
| number Turbomachinery performance option specified from config file. More... | |
| unsigned short | GetnMarker_Shroud (void) |
| Get number of shroud markers. More... | |
| string | GetMarker_Shroud (unsigned short val_marker) |
| Get the marker shroud. More... | |
| unsigned short | GetnMarker_TurboPerformance (void) |
| number Turbomachinery performance option specified from config file. More... | |
| unsigned short | Get_nSpanWiseSections_User (void) |
| number span-wise sections to compute 3D BC and performance for turbomachinery specified by the user. More... | |
| unsigned short | GetnSpanWiseSections (void) |
| number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| void | SetnSpanMaxAllZones (unsigned short val_nSpna_max) |
| set number of maximum span-wise sections among all zones . More... | |
| unsigned short | GetnSpanMaxAllZones (void) |
| number span-wise sections to compute performance for turbomachinery. More... | |
| void | SetnSpanWiseSections (unsigned short nSpan) |
| set number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| unsigned short | GetnSpan_iZones (unsigned short iZone) |
| set number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| void | SetnSpan_iZones (unsigned short nSpan, unsigned short iZone) |
| set number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| string | GetMarker_TurboPerf_BoundIn (unsigned short index) |
| get inlet bounds name for Turbomachinery performance calculation. More... | |
| string | GetMarker_TurboPerf_BoundOut (unsigned short index) |
| get outlet bounds name for Turbomachinery performance calculation. More... | |
| unsigned short | GetKind_TurboPerf (unsigned short index) |
| get marker kind for Turbomachinery performance calculation. More... | |
| string | GetMarker_PerBound (unsigned short val_marker) |
| get outlet bounds name for Turbomachinery performance calculation. More... | |
| unsigned short | GetKind_Engine_Inflow (void) |
| Get the kind of inlet boundary condition treatment (total conditions or mass flow). More... | |
| unsigned short | GetKind_ActDisk (void) |
| Get the kind of inlet boundary condition treatment (total conditions or mass flow). More... | |
| unsigned short | GetnLocationStations (void) |
| Get the number of sections. More... | |
| unsigned short | GetnWingStations (void) |
| Get the number of sections for computing internal volume. More... | |
| su2double | GetGeo_Waterline_Location (void) |
| Get the location of the waterline. More... | |
| bool | GetHold_GridFixed (void) |
| Provides information about the the nodes that are going to be moved on a deformation volumetric grid deformation. More... | |
| unsigned short | GetKind_ObjFunc (void) |
| Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More... | |
| unsigned short | GetKind_ObjFunc (unsigned short val_obj) |
| Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More... | |
| su2double | GetWeight_ObjFunc (unsigned short val_obj) |
| Get the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More... | |
| void | SetWeight_ObjFunc (unsigned short val_obj, su2double val) |
| Set the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More... | |
| su2double | GetCoeff_ObjChainRule (unsigned short iVar) |
| Get the coefficients of the objective defined by the chain rule with primitive variables. More... | |
| bool | GetComboObj (void) |
| Get the flag indicating whether to comput a combined objective. More... | |
| unsigned short | GetKind_SensSmooth (void) |
| Get the kind of sensitivity smoothing technique. More... | |
| unsigned short | GetUnsteady_Simulation (void) |
| Provides information about the time integration, and change the write in the output files information about the iteration. More... | |
| unsigned short | GetnReactions (void) |
| Provides the number of chemical reactions in the chemistry model. More... | |
| su2double | GetArrheniusCoeff (unsigned short iReaction) |
| Provides the number of chemical reactions in the chemistry model. More... | |
| su2double | GetArrheniusEta (unsigned short iReaction) |
| Provides the number of chemical reactions in the chemistry model. More... | |
| su2double | GetArrheniusTheta (unsigned short iReaction) |
| Provides the number of chemical reactions in the chemistry model. More... | |
| su2double * | GetRxnTcf_a (void) |
| Provides the rate controlling temperature exponents for chemistry. More... | |
| su2double * | GetRxnTcf_b (void) |
| Provides the rate controlling temperature exponents for chemistry. More... | |
| su2double * | GetRxnTcb_a (void) |
| Provides the rate controlling temperature exponents for chemistry. More... | |
| su2double * | GetRxnTcb_b (void) |
| Provides the rate controlling temperature exponents for chemistry. More... | |
| su2double * | GetDissociationPot (void) |
| Dissociation potential of species. More... | |
| su2double * | GetRotationModes (void) |
| Provides the number of rotational modes of energy storage. More... | |
| su2double * | GetCharVibTemp (void) |
| Provides the characteristic vibrational temperature for calculating e_vib. More... | |
| su2double ** | GetCharElTemp (void) |
| Provides the characteristic electronic temperature for calculating e_el. More... | |
| su2double ** | GetElDegeneracy (void) |
| Provides the degeneracy of electron states for calculating e_el. More... | |
| unsigned short * | GetnElStates (void) |
| Provides number electron states for calculating e_el. More... | |
| su2double * | GetRefTemperature (void) |
| Provides the thermodynamic reference temperatures from the JANAF tables. More... | |
| su2double | GetCharVibTemp (unsigned short iSpecies) |
| Provides the characteristic vibrational temperature for calculating e_vib. More... | |
| su2double * | GetMolar_Mass (void) |
| Provides the molar mass of each species present in multi species fluid. More... | |
| su2double | GetMolar_Mass (unsigned short iSpecies) |
| Provides the molar mass of each species present in multi species fluid. More... | |
| unsigned short | GetnMonatomics (void) |
| Retrieves the number of monatomic species in the multicomponent gas. More... | |
| unsigned short | GetnDiatomics (void) |
| Retrieves the number of monatomic species in the multicomponent gas. More... | |
| su2double | GetInitial_Gas_Composition (unsigned short iSpecies) |
| Provides the molar mass of each species present in multi species fluid. More... | |
| su2double * | GetEnthalpy_Formation (void) |
| Provides the formation enthalpy of the specified species at standard conditions. More... | |
| su2double | GetEnthalpy_Formation (unsigned short iSpecies) |
| Provides the formation enthalpy of the specified species at standard conditions. More... | |
| bool | GetRestart (void) |
| Provides the restart information. More... | |
| bool | GetWrt_Binary_Restart (void) |
| Flag for whether binary SU2 native restart files are written. More... | |
| bool | GetRead_Binary_Restart (void) |
| Flag for whether binary SU2 native restart files are read. More... | |
| unsigned short | GetnVar (void) |
| Provides the number of varaibles. More... | |
| unsigned short | GetnZone (void) |
| Provides the number of varaibles. More... | |
| unsigned short | GetiZone (void) |
| Provides the number of varaibles. More... | |
| bool | GetRestart_Flow (void) |
| For some problems like adjoint or the linearized equations it is necessary to restart the flow solution. More... | |
| bool | GetIonization (void) |
| Indicates whether electron gas is present in the gas mixture. More... | |
| bool | GetEquivArea (void) |
| Information about computing and plotting the equivalent area distribution. More... | |
| bool | GetInvDesign_Cp (void) |
| Information about computing and plotting the equivalent area distribution. More... | |
| bool | GetInvDesign_HeatFlux (void) |
| Information about computing and plotting the equivalent area distribution. More... | |
| string | GetMesh_FileName (void) |
| Get name of the input grid. More... | |
| string | GetMesh_Out_FileName (void) |
| Get name of the output grid, this parameter is important for grid adaptation and deformation. More... | |
| string | GetSolution_FlowFileName (void) |
| Get the name of the file with the solution of the flow problem. More... | |
| string | GetSolution_AdjFileName (void) |
| Get the name of the file with the solution of the adjoint flow problem with drag objective function. More... | |
| string | GetSolution_FEMFileName (void) |
| Get the name of the file with the solution of the structural problem. More... | |
| string | GetSolution_AdjFEMFileName (void) |
| Get the name of the file with the solution of the adjoint structural problem. More... | |
| string | GetResidual_FileName (void) |
| Get the name of the file with the residual of the problem. More... | |
| unsigned short | GetMesh_FileFormat (void) |
| Get the format of the input/output grid. More... | |
| unsigned short | GetOutput_FileFormat (void) |
| Get the format of the output solution. More... | |
| unsigned short | GetActDisk_Jump (void) |
| Get the format of the output solution. More... | |
| string | GetConv_FileName (void) |
| Get the name of the file with the convergence history of the problem. More... | |
| string | GetConv_FileName_FSI (void) |
| Get the name of the file with the convergence history of the problem for FSI applications. More... | |
| string | GetBreakdown_FileName (void) |
| Get the name of the file with the forces breakdown of the problem. More... | |
| string | GetFlow_FileName (void) |
| Get the name of the file with the flow variables. More... | |
| string | GetStructure_FileName (void) |
| Get the name of the file with the structure variables. More... | |
| string | GetSurfStructure_FileName (void) |
| Get the name of the file with the structure variables. More... | |
| string | GetAdjStructure_FileName (void) |
| Get the name of the file with the adjoint structure variables. More... | |
| string | GetAdjSurfStructure_FileName (void) |
| Get the name of the file with the adjoint structure variables. More... | |
| string | GetSurfHeat_FileName (void) |
| Get the name of the file with the structure variables. More... | |
| string | GetHeat_FileName (void) |
| Get the name of the file with the wave variables. More... | |
| string | GetRestart_HeatFileName (void) |
| Get the name of the restart file for the heat variables. More... | |
| string | GetMultizone_FileName (string val_filename, int val_iZone) |
| Append the zone index to the restart or the solution files. More... | |
| string | GetMultizone_HistoryFileName (string val_filename, int val_iZone) |
| Append the zone index to the restart or the solution files. More... | |
| string | GetMultiInstance_FileName (string val_filename, int val_iInst) |
| Append the instance index to the restart or the solution files. More... | |
| string | GetMultiInstance_HistoryFileName (string val_filename, int val_iInst) |
| Append the instance index to the restart or the solution files. More... | |
| string | GetRestart_FlowFileName (void) |
| Get the name of the restart file for the flow variables. More... | |
| string | GetRestart_AdjFileName (void) |
| Get the name of the restart file for the adjoint variables (drag objective function). More... | |
| string | GetRestart_FEMFileName (void) |
| Get the name of the restart file for the structural variables. More... | |
| string | GetRestart_AdjFEMFileName (void) |
| Get the name of the restart file for the structural adjoint variables. More... | |
| string | GetAdj_FileName (void) |
| Get the name of the file with the adjoint variables. More... | |
| string | GetObjFunc_Grad_FileName (void) |
| Get the name of the file with the gradient of the objective function. More... | |
| string | GetObjFunc_Value_FileName (void) |
| Get the name of the file with the gradient of the objective function. More... | |
| string | GetSurfFlowCoeff_FileName (void) |
| Get the name of the file with the surface information for the flow problem. More... | |
| string | GetSurfAdjCoeff_FileName (void) |
| Get the name of the file with the surface information for the adjoint problem. More... | |
| string | GetSurfSens_FileName (void) |
| Get the name of the file with the surface sensitivity (discrete adjoint). More... | |
| string | GetVolSens_FileName (void) |
| Get the name of the file with the volume sensitivity (discrete adjoint). More... | |
| string | GetUnsteady_FileName (string val_filename, int val_iter) |
| Augment the input filename with the iteration number for an unsteady file. More... | |
| string | GetObjFunc_Extension (string val_filename) |
| Append the input filename string with the appropriate objective function extension. More... | |
| unsigned short | GetResidual_Criteria_FEM (void) |
| Get the criteria for structural residual (relative/absolute). More... | |
| unsigned short | GetResidual_Func_Flow (void) |
| Get functional that is going to be used to evaluate the residual flow convergence. More... | |
| unsigned short | GetCauchy_Func_Flow (void) |
| Get functional that is going to be used to evaluate the flow convergence. More... | |
| unsigned short | GetCauchy_Func_AdjFlow (void) |
| Get functional that is going to be used to evaluate the adjoint flow convergence. More... | |
| unsigned short | GetCauchy_Elems (void) |
| Get the number of iterations that are considered in the Cauchy convergence criteria. More... | |
| unsigned long | GetStartConv_Iter (void) |
| Get the number of iterations that are not considered in the convergence criteria. More... | |
| su2double | GetCauchy_Eps (void) |
| Get the value of convergence criteria for the Cauchy method in the direct, adjoint or linearized problem. More... | |
| su2double | GetDelta_UnstTimeND (void) |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| su2double | GetTotal_UnstTimeND (void) |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| su2double | GetDelta_UnstTime (void) |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| void | SetDelta_UnstTimeND (su2double val_delta_unsttimend) |
| Set the value of the unsteadty time step using the CFL number. More... | |
| su2double | GetTotal_UnstTime (void) |
| If we are performing an unsteady simulation, this is the value of max physical time for which we run the simulation. More... | |
| su2double | GetCurrent_UnstTime (void) |
| If we are performing an unsteady simulation, this is the value of current time. More... | |
| bool | GetSubsonicEngine (void) |
| Divide the rectbles and hexahedron. More... | |
| bool | GetActDisk_DoubleSurface (void) |
| Actuator disk defined with a double surface. More... | |
| bool | GetEngine_HalfModel (void) |
| Only halg of the engine is in the compputational grid. More... | |
| bool | GetActDisk_SU2_DEF (void) |
| Actuator disk defined with a double surface. More... | |
| su2double | GetDV_Value (unsigned short val_dv, unsigned short val_val=0) |
| Value of the design variable step, we use this value in design problems. More... | |
| void | SetDV_Value (unsigned short val_dv, unsigned short val_ind, su2double val) |
| Set the value of the design variable step, we use this value in design problems. More... | |
| bool | GetGrid_Movement (void) |
| Get information about the grid movement. More... | |
| unsigned short | GetKind_GridMovement (unsigned short val_iZone) |
| Get the type of dynamic mesh motion. More... | |
| void | SetKind_GridMovement (unsigned short val_iZone, unsigned short motion_Type) |
| Set the type of dynamic mesh motion. More... | |
| su2double | GetMach_Motion (void) |
| Get the mach number based on the mesh velocity and freestream quantities. More... | |
| su2double | GetMotion_Origin_X (unsigned short val_iZone) |
| Get x-coordinate of the mesh motion origin. More... | |
| su2double | GetMotion_Origin_Y (unsigned short val_iZone) |
| Get y-coordinate of the mesh motion origin. More... | |
| su2double | GetMotion_Origin_Z (unsigned short val_iZone) |
| Get z-coordinate of the mesh motion origin. More... | |
| void | SetMotion_Origin_X (unsigned short val_iZone, su2double val_origin) |
| Set x-coordinate of the mesh motion origin. More... | |
| void | SetMotion_Origin_Y (unsigned short val_iZone, su2double val_origin) |
| Set y-coordinate of the mesh motion origin. More... | |
| void | SetMotion_Origin_Z (unsigned short val_iZone, su2double val_origin) |
| Set z-coordinate of the mesh motion origin. More... | |
| su2double | GetTranslation_Rate_X (unsigned short val_iZone) |
| Get the translational velocity of the mesh in the x-direction. More... | |
| su2double | GetTranslation_Rate_Y (unsigned short val_iZone) |
| Get the translational velocity of the mesh in the y-direction. More... | |
| su2double | GetTranslation_Rate_Z (unsigned short val_iZone) |
| Get the translational velocity of the mesh in the z-direction. More... | |
| su2double | GetRotation_Rate_X (unsigned short val_iZone) |
| Get the angular velocity of the mesh about the x-axis. More... | |
| su2double | GetRotation_Rate_Y (unsigned short val_iZone) |
| Get the angular velocity of the mesh about the y-axis. More... | |
| su2double | GetRotation_Rate_Z (unsigned short val_iZone) |
| Get the angular velocity of the mesh about the z-axis. More... | |
| su2double | GetFinalRotation_Rate_Z (unsigned short val_iZone) |
| Get the angular velocity of the mesh about the z-axis. More... | |
| void | SetRotation_Rate_Z (su2double newRotation_Rate_Z, unsigned short val_iZone) |
| Set the angular velocity of the mesh about the z-axis. More... | |
| su2double | GetPitching_Omega_X (unsigned short val_iZone) |
| Get the angular frequency of a mesh pitching about the x-axis. More... | |
| su2double | GetPitching_Omega_Y (unsigned short val_iZone) |
| Get the angular frequency of a mesh pitching about the y-axis. More... | |
| su2double | GetPitching_Omega_Z (unsigned short val_iZone) |
| Get the angular frequency of a mesh pitching about the z-axis. More... | |
| su2double | GetPitching_Ampl_X (unsigned short val_iZone) |
| Get the pitching amplitude about the x-axis. More... | |
| su2double | GetPitching_Ampl_Y (unsigned short val_iZone) |
| Get the pitching amplitude about the y-axis. More... | |
| su2double | GetPitching_Ampl_Z (unsigned short val_iZone) |
| Get the pitching amplitude about the z-axis. More... | |
| su2double | GetPitching_Phase_X (unsigned short val_iZone) |
| Get the pitching phase offset about the x-axis. More... | |
| su2double | GetPitching_Phase_Y (unsigned short val_iZone) |
| Get the pitching phase offset about the y-axis. More... | |
| su2double | GetPitching_Phase_Z (unsigned short val_iZone) |
| Get the pitching phase offset about the z-axis. More... | |
| su2double | GetPlunging_Omega_X (unsigned short val_iZone) |
| Get the angular frequency of a mesh plunging in the x-direction. More... | |
| su2double | GetPlunging_Omega_Y (unsigned short val_iZone) |
| Get the angular frequency of a mesh plunging in the y-direction. More... | |
| su2double | GetPlunging_Omega_Z (unsigned short val_iZone) |
| Get the angular frequency of a mesh plunging in the z-direction. More... | |
| su2double | GetPlunging_Ampl_X (unsigned short val_iZone) |
| Get the plunging amplitude in the x-direction. More... | |
| su2double | GetPlunging_Ampl_Y (unsigned short val_iZone) |
| Get the plunging amplitude in the y-direction. More... | |
| su2double | GetPlunging_Ampl_Z (unsigned short val_iZone) |
| Get the plunging amplitude in the z-direction. More... | |
| su2double * | GetOmega_HB (void) |
| Get the Harmonic Balance frequency pointer. More... | |
| bool | GetHB_Precondition (void) |
| Get if harmonic balance source term is to be preconditioned. More... | |
| unsigned short | GetMoveMotion_Origin (unsigned short val_marker) |
| Get if we should update the motion origin. More... | |
| su2double | GetminTurkelBeta () |
| Get the minimum value of Beta for Roe-Turkel preconditioner. More... | |
| su2double | GetmaxTurkelBeta () |
| Get the minimum value of Beta for Roe-Turkel preconditioner. More... | |
| bool | GetAdiabaticWall (void) |
| Get information about the adibatic wall condition. More... | |
| bool | GetIsothermalWall (void) |
| Get information about the isothermal wall condition. More... | |
| bool | Low_Mach_Preconditioning (void) |
| Get information about the Low Mach Preconditioning. More... | |
| bool | Low_Mach_Correction (void) |
| Get information about the Low Mach Correction. More... | |
| bool | GetPoissonSolver (void) |
| Get information about the poisson solver condition. More... | |
| bool | GetGravityForce (void) |
| Get information about the gravity force. More... | |
| bool | GetBody_Force (void) |
| Get information about the body force. More... | |
| su2double * | GetBody_Force_Vector (void) |
| Get a pointer to the body force vector. More... | |
| bool | GetRotating_Frame (void) |
| Get information about the rotational frame. More... | |
| bool | GetAxisymmetric (void) |
| Get information about the axisymmetric frame. More... | |
| bool | GetDebugMode (void) |
| Get information about the axisymmetric frame. More... | |
| bool | GetAdaptBoundary (void) |
| Get information about there is a smoothing of the grid coordinates. More... | |
| bool | GetSmoothNumGrid (void) |
| Get information about there is a smoothing of the grid coordinates. More... | |
| void | SetSmoothNumGrid (bool val_smoothnumgrid) |
| Set information about there is a smoothing of the grid coordinates. More... | |
| void | SubtractFinestMesh (void) |
| Subtract one to the index of the finest grid (full multigrid strategy). More... | |
| unsigned short | GetDesign_Variable (unsigned short val_dv) |
| Obtain the kind of design variable. More... | |
| string | GetTranspTag (unsigned short val_dv) |
| Obtain the marker of a transpiration DV. More... | |
| bool | GetTranspiration_Objective (void) |
| Provides the transpiration objective information. More... | |
| bool | GetBuffet_Monitoring (void) |
| Provides the buffet monitoring information. More... | |
| su2double | GetBuffet_k (void) |
| Get the buffet sensor sharpness coefficient. More... | |
| su2double | GetBuffet_lambda (void) |
| Get the buffet sensor offset parameter. More... | |
| unsigned short | GetConvCriteria (void) |
| Obtain the kind of convergence criteria to establish the convergence of the CFD code. More... | |
| unsigned short | GetMarker_CfgFile_TagBound (string val_marker) |
| Get the index in the config information of the marker val_marker. More... | |
| string | GetMarker_CfgFile_TagBound (unsigned short val_marker) |
| Get the name in the config information of the marker number val_marker. More... | |
| unsigned short | GetMarker_CfgFile_KindBC (string val_marker) |
| Get the boundary information (kind of boundary) in the config information of the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Monitoring (string val_marker) |
| Get the monitoring information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_GeoEval (string val_marker) |
| Get the monitoring information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Designing (string val_marker) |
| Get the monitoring information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Plotting (string val_marker) |
| Get the plotting information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Analyze (string val_marker) |
| Get the plotting information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_ZoneInterface (string val_marker) |
| Get the FSI interface information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Turbomachinery (string val_marker) |
| Get the TurboPerformance information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_TurbomachineryFlag (string val_marker) |
| Get the TurboPerformance flag information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_MixingPlaneInterface (string val_marker) |
| Get the MixingPlane interface information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_DV (string val_marker) |
| Get the DV information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Moving (string val_marker) |
| Get the motion information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_PyCustom (string val_marker) |
| Get the Python customization information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_PerBound (string val_marker) |
| Get the periodic information from the config definition of the marker val_marker. More... | |
| int | GetMarker_ZoneInterface (string val_marker) |
| Get the name of the marker val_marker. More... | |
| bool | GetContinuous_Adjoint (void) |
| Determines if problem is adjoint. More... | |
| bool | GetViscous (void) |
| Determines if problem is viscous. More... | |
| unsigned short | GetContainerPosition (unsigned short val_eqsystem) |
| Provides the index of the solution in the container. More... | |
| su2double | GetOrderMagResidual (void) |
| Value of the order of magnitude reduction of the residual. More... | |
| su2double | GetMinLogResidual (void) |
| Value of the minimum residual value (log10 scale). More... | |
| su2double | GetOrderMagResidualFSI (void) |
| Value of the order of magnitude reduction of the residual for FSI applications. More... | |
| su2double | GetMinLogResidualFSI (void) |
| Value of the minimum residual value for FSI applications (log10 scale). More... | |
| su2double | GetOrderMagResidual_BGS_F (void) |
| Value of the order of magnitude reduction of the flow residual for BGS applications. More... | |
| su2double | GetMinLogResidual_BGS_F (void) |
| Value of the minimum flow residual value for BGS applications (log10 scale). More... | |
| su2double | GetOrderMagResidual_BGS_S (void) |
| Value of the order of magnitude reduction of the flow residual for BGS applications. More... | |
| su2double | GetMinLogResidual_BGS_S (void) |
| Value of the minimum flow residual value for BGS applications (log10 scale). More... | |
| su2double | GetResidual_FEM_UTOL (void) |
| Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale). More... | |
| su2double | GetResidual_FEM_RTOL (void) |
| Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale). More... | |
| su2double | GetResidual_FEM_ETOL (void) |
| Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale). More... | |
| su2double | GetCriteria_FEM_ADJ (void) |
| Value of the maximum objective function for FEM elasticity adjoint (log10 scale). More... | |
| su2double | GetDamp_Engine_Inflow (void) |
| Value of the damping factor for the engine inlet bc. More... | |
| su2double | GetDamp_Engine_Exhaust (void) |
| Value of the damping factor for the engine exhaust inlet bc. More... | |
| su2double | GetDamp_Res_Restric (void) |
| Value of the damping factor for the residual restriction. More... | |
| su2double | GetDamp_Correc_Prolong (void) |
| Value of the damping factor for the correction prolongation. More... | |
| su2double | GetPosition_Plane (void) |
| Value of the position of the Near Field (y coordinate for 2D, and z coordinate for 3D). More... | |
| su2double | GetWeightCd (void) |
| Value of the weight of the drag coefficient in the Sonic Boom optimization. More... | |
| void | SetdNetThrust_dBCThrust (su2double val_dnetthrust_dbcthrust) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetFixAzimuthalLine (void) |
| Value of the azimuthal line to fix due to a misalignments of the nearfield. More... | |
| su2double | GetdCD_dCMy (void) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetCM_Target (void) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetdCD_dCL (void) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCD_dCL (su2double val_dcd_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetdCMx_dCL (void) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCMx_dCL (su2double val_dcmx_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetdCMy_dCL (void) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCMy_dCL (su2double val_dcmy_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetdCMz_dCL (void) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCMz_dCL (su2double val_dcmz_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCL_dAlpha (su2double val_dcl_dalpha) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCM_diH (su2double val_dcm_dhi) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCD_dCMy (su2double val_dcd_dcmy) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetCL_Target (void) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetGlobalParam (unsigned short val_solver, unsigned short val_system, unsigned long val_extiter) |
| Set the global parameters of each simulation for each runtime system. More... | |
| su2double * | GetPeriodicRotCenter (string val_marker) |
| Center of rotation for a rotational periodic boundary. More... | |
| su2double * | GetPeriodicRotAngles (string val_marker) |
| Angles of rotation for a rotational periodic boundary. More... | |
| su2double * | GetPeriodicTranslation (string val_marker) |
| Translation vector for a rotational periodic boundary. More... | |
| unsigned short | GetMarker_Periodic_Donor (string val_marker) |
| Get the rotationally periodic donor marker for boundary val_marker. More... | |
| su2double | GetActDisk_NetThrust (string val_marker) |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Power (string val_marker) |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_MassFlow (string val_marker) |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Mach (string val_marker) |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Force (string val_marker) |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_BCThrust (string val_marker) |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_BCThrust_Old (string val_marker) |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Area (string val_marker) |
| Get the tip radius of th actuator disk. More... | |
| su2double | GetActDisk_ReverseMassFlow (string val_marker) |
| Get the tip radius of th actuator disk. More... | |
| su2double | GetActDisk_PressJump (string val_marker, unsigned short val_index) |
| Get the thrust corffient of the actuator disk. More... | |
| su2double | GetActDisk_TempJump (string val_marker, unsigned short val_index) |
| Get the thrust corffient of the actuator disk. More... | |
| su2double | GetActDisk_Omega (string val_marker, unsigned short val_index) |
| Get the rev / min of the actuator disk. More... | |
| unsigned short | GetMarker_CfgFile_ActDiskOutlet (string val_marker) |
| Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet). More... | |
| unsigned short | GetMarker_CfgFile_EngineExhaust (string val_marker) |
| Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet). More... | |
| unsigned short | GetMarker_Moving (string val_marker) |
| Get the internal index for a moving boundary val_marker. More... | |
| string | GetMarker_Moving_TagBound (unsigned short val_marker) |
| Get the name of the surface defined in the geometry file. More... | |
| string | GetMarker_PyCustom_TagBound (unsigned short val_marker) |
| Get the name of the surface defined in the geometry file. More... | |
| string | GetMarker_Analyze_TagBound (unsigned short val_marker) |
| Get the name of the surface defined in the geometry file. More... | |
| void | SetnPeriodicIndex (unsigned short val_index) |
| Set the total number of SEND_RECEIVE periodic transformations. More... | |
| unsigned short | GetnPeriodicIndex (void) |
| Get the total number of SEND_RECEIVE periodic transformations. More... | |
| void | SetPeriodicCenter (unsigned short val_index, su2double *center) |
| Set the rotation center for a periodic transformation. More... | |
| su2double * | GetPeriodicCenter (unsigned short val_index) |
| Get the rotation center for a periodic transformation. More... | |
| void | SetPeriodicRotation (unsigned short val_index, su2double *rotation) |
| Set the rotation angles for a periodic transformation. More... | |
| su2double * | GetPeriodicRotation (unsigned short val_index) |
| Get the rotation angles for a periodic transformation. More... | |
| void | SetPeriodicTranslate (unsigned short val_index, su2double *translate) |
| Set the translation vector for a periodic transformation. More... | |
| su2double * | GetPeriodicTranslate (unsigned short val_index) |
| Get the translation vector for a periodic transformation. More... | |
| su2double | GetExhaust_Temperature_Target (string val_index) |
| Get the total temperature at a nacelle boundary. More... | |
| su2double | GetInlet_Ttotal (string val_index) |
| Get the total temperature at an inlet boundary. More... | |
| su2double | GetInlet_Temperature (string val_index) |
| Get the temperature at a supersonic inlet boundary. More... | |
| su2double | GetInlet_Pressure (string val_index) |
| Get the pressure at a supersonic inlet boundary. More... | |
| su2double * | GetInlet_Velocity (string val_index) |
| Get the velocity vector at a supersonic inlet boundary. More... | |
| su2double | GetDirichlet_Value (string val_index) |
| Get the fixed value at the Dirichlet boundary. More... | |
| bool | GetDirichlet_Boundary (string val_index) |
| Get whether this is a Dirichlet or a Neumann boundary. More... | |
| su2double | GetInlet_Ptotal (string val_index) |
| Get the total pressure at an inlet boundary. More... | |
| void | SetInlet_Ptotal (su2double val_pressure, string val_marker) |
| Set the total pressure at an inlet boundary. More... | |
| su2double | GetExhaust_Pressure_Target (string val_index) |
| Get the total pressure at an nacelle boundary. More... | |
| su2double | GetCFLRedCoeff_Turb (void) |
| Value of the CFL reduction in LevelSet problems. More... | |
| su2double * | GetInlet_FlowDir (string val_index) |
| Get the flow direction unit vector at an inlet boundary. More... | |
| su2double | GetOutlet_Pressure (string val_index) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetOutlet_Pressure (su2double val_pressure, string val_marker) |
| Set the back pressure (static) at an outlet boundary. More... | |
| su2double | GetRiemann_Var1 (string val_marker) |
| Get the var 1 at Riemann boundary. More... | |
| su2double | GetRiemann_Var2 (string val_marker) |
| Get the var 2 at Riemann boundary. More... | |
| su2double * | GetRiemann_FlowDir (string val_marker) |
| Get the Flowdir at Riemann boundary. More... | |
| unsigned short | GetKind_Data_Riemann (string val_marker) |
| Get Kind Data of Riemann boundary. More... | |
| su2double | GetGiles_Var1 (string val_marker) |
| Get the var 1 for the Giels BC. More... | |
| su2double | GetGiles_Var2 (string val_marker) |
| Get the var 2 for the Giles boundary. More... | |
| su2double * | GetGiles_FlowDir (string val_marker) |
| Get the Flowdir for the Giles BC. More... | |
| unsigned short | GetKind_Data_Giles (string val_marker) |
| Get Kind Data for the Giles BC. More... | |
| void | SetGiles_Var1 (su2double newVar1, string val_marker) |
| Set the var 1 for Giles BC. More... | |
| su2double | GetGiles_RelaxFactorAverage (string val_marker) |
| Get the relax factor for the average component for the Giles BC. More... | |
| su2double | GetGiles_RelaxFactorFourier (string val_marker) |
| Get the relax factor for the fourier component for the Giles BC. More... | |
| su2double | GetPressureOut_BC () |
| Get the outlet pressure imposed as BC for internal flow. More... | |
| void | SetPressureOut_BC (su2double val_press) |
| Set the outlet pressure imposed as BC for internal flow. More... | |
| su2double | GetIncInlet_BC () |
| Get the inlet velocity or pressure imposed for incompressible flow. More... | |
| void | SetIncInlet_BC (su2double val_in) |
| Set the inlet velocity or pressure imposed as BC for incompressible flow. More... | |
| su2double | GetIncTemperature_BC () |
| Get the inlet temperature imposed as BC for incompressible flow. More... | |
| void | SetIncTemperature_BC (su2double val_temperature) |
| Set the inlet temperature imposed as BC for incompressible flow. More... | |
| su2double | GetIncPressureOut_BC () |
| Get the outlet pressure imposed as BC for incompressible flow. More... | |
| void | SetIncPressureOut_BC (su2double val_pressure) |
| Set the outlet pressure imposed as BC for incompressible flow. More... | |
| su2double | GetTotalPressureIn_BC () |
| Get the inlet total pressure imposed as BC for internal flow. More... | |
| su2double | GetTotalTemperatureIn_BC () |
| Get the inlet total temperature imposed as BC for internal flow. More... | |
| void | SetTotalTemperatureIn_BC (su2double val_temp) |
| Set the inlet total temperature imposed as BC for internal flow. More... | |
| su2double | GetFlowAngleIn_BC () |
| Get the inlet flow angle imposed as BC for internal flow. More... | |
| su2double | GetIsothermal_Temperature (string val_index) |
| Get the wall temperature (static) at an isothermal boundary. More... | |
| su2double | GetWall_HeatFlux (string val_index) |
| Get the wall heat flux on a constant heat flux boundary. More... | |
| void | GetTranspirationParams (string val_marker, su2double &x0, su2double &x1, su2double &x2, su2double &x3, su2double &y0, su2double &y1, su2double &y2, su2double &y3, su2double &eps0, su2double &eps1, su2double &eps2, su2double &eps3) |
| Get the wall transpiration parameters. More... | |
| void | SetTranspirationParams_DV () |
| Set the transpiration params using DV values. More... | |
| string | GetTranspirationFileName () |
| Get the name of file containing all transpirations. More... | |
| unsigned short | GetWallFunction_Treatment (string val_marker) |
| Get the wall function treatment for the given boundary marker. More... | |
| unsigned short * | GetWallFunction_IntInfo (string val_marker) |
| Get the additional integer info for the wall function treatment for the given boundary marker. More... | |
| su2double * | GetWallFunction_DoubleInfo (string val_marker) |
| Get the additional double info for the wall function treatment for the given boundary marker. More... | |
| su2double | GetEngineInflow_Target (string val_marker) |
| Get the target (pressure, massflow, etc) at an engine inflow boundary. More... | |
| su2double | GetInflow_Mach (string val_marker) |
| Get the fan face Mach number at an engine inflow boundary. More... | |
| su2double | GetInflow_Pressure (string val_marker) |
| Get the back pressure (static) at an engine inflow boundary. More... | |
| su2double | GetInflow_MassFlow (string val_marker) |
| Get the mass flow rate at an engine inflow boundary. More... | |
| su2double | GetInflow_ReverseMassFlow (string val_marker) |
| Get the percentage of reverse flow at an engine inflow boundary. More... | |
| su2double | GetInflow_ReverseMassFlow (unsigned short val_marker) |
| Get the percentage of reverse flow at an engine inflow boundary. More... | |
| su2double | GetInflow_TotalPressure (string val_marker) |
| Get the total pressure at an engine inflow boundary. More... | |
| su2double | GetInflow_Temperature (string val_marker) |
| Get the temperature (static) at an engine inflow boundary. More... | |
| su2double | GetInflow_TotalTemperature (string val_marker) |
| Get the total temperature at an engine inflow boundary. More... | |
| su2double | GetInflow_RamDrag (string val_marker) |
| Get the ram drag at an engine inflow boundary. More... | |
| su2double | GetInflow_Force (string val_marker) |
| Get the force balance at an engine inflow boundary. More... | |
| su2double | GetInflow_Power (string val_marker) |
| Get the power at an engine inflow boundary. More... | |
| su2double | GetExhaust_Pressure (string val_marker) |
| Get the back pressure (static) at an engine exhaust boundary. More... | |
| su2double | GetExhaust_Temperature (string val_marker) |
| Get the temperature (static) at an engine exhaust boundary. More... | |
| su2double | GetExhaust_MassFlow (string val_marker) |
| Get the massflow at an engine exhaust boundary. More... | |
| su2double | GetExhaust_TotalPressure (string val_marker) |
| Get the total pressure at an engine exhaust boundary. More... | |
| su2double | GetExhaust_TotalTemperature (string val_marker) |
| Get the total temperature at an engine exhaust boundary. More... | |
| su2double | GetExhaust_GrossThrust (string val_marker) |
| Get the gross thrust at an engine exhaust boundary. More... | |
| su2double | GetExhaust_Force (string val_marker) |
| Get the force balance at an engine exhaust boundary. More... | |
| su2double | GetExhaust_Power (string val_marker) |
| Get the power at an engine exhaust boundary. More... | |
| void | SetInflow_Mach (unsigned short val_imarker, su2double val_fanface_mach) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetInflow_Pressure (unsigned short val_imarker, su2double val_fanface_pressure) |
| Set the fan face static pressure at an engine inflow boundary. More... | |
| void | SetInflow_MassFlow (unsigned short val_imarker, su2double val_fanface_massflow) |
| Set the massflow at an engine inflow boundary. More... | |
| void | SetInflow_ReverseMassFlow (unsigned short val_imarker, su2double val_fanface_reversemassflow) |
| Set the reverse flow at an engine inflow boundary. More... | |
| void | SetInflow_TotalPressure (unsigned short val_imarker, su2double val_fanface_totalpressure) |
| Set the fan face total pressure at an engine inflow boundary. More... | |
| void | SetInflow_Temperature (unsigned short val_imarker, su2double val_fanface_temperature) |
| Set the fan face static temperature at an engine inflow boundary. More... | |
| void | SetInflow_TotalTemperature (unsigned short val_imarker, su2double val_fanface_totaltemperature) |
| Set the fan face total temperature at an engine inflow boundary. More... | |
| void | SetInflow_RamDrag (unsigned short val_imarker, su2double val_fanface_ramdrag) |
| Set the ram drag temperature at an engine inflow boundary. More... | |
| void | SetInflow_Force (unsigned short val_imarker, su2double val_fanface_force) |
| Set the force balance at an engine inflow boundary. More... | |
| void | SetInflow_Power (unsigned short val_imarker, su2double val_fanface_power) |
| Set the power at an engine inflow boundary. More... | |
| void | SetExhaust_Pressure (unsigned short val_imarker, su2double val_exhaust_pressure) |
| Set the back pressure (static) at an engine exhaust boundary. More... | |
| void | SetExhaust_Temperature (unsigned short val_imarker, su2double val_exhaust_temp) |
| Set the temperature (static) at an engine exhaust boundary. More... | |
| void | SetExhaust_MassFlow (unsigned short val_imarker, su2double val_exhaust_massflow) |
| Set the back pressure (static) at an engine exhaust boundary. More... | |
| void | SetExhaust_TotalPressure (unsigned short val_imarker, su2double val_exhaust_totalpressure) |
| Set the back pressure (total) at an engine exhaust boundary. More... | |
| void | SetExhaust_TotalTemperature (unsigned short val_imarker, su2double val_exhaust_totaltemp) |
| Set the total temperature at an engine exhaust boundary. More... | |
| void | SetExhaust_GrossThrust (unsigned short val_imarker, su2double val_exhaust_grossthrust) |
| Set the gross thrust at an engine exhaust boundary. More... | |
| void | SetExhaust_Force (unsigned short val_imarker, su2double val_exhaust_force) |
| Set the force balance at an engine exhaust boundary. More... | |
| void | SetExhaust_Power (unsigned short val_imarker, su2double val_exhaust_power) |
| Set the power at an engine exhaust boundary. More... | |
| void | SetEngine_Mach (unsigned short val_imarker, su2double val_engine_mach) |
| Set the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_Force (unsigned short val_imarker, su2double val_engine_force) |
| Set the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_Power (unsigned short val_imarker, su2double val_engine_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_NetThrust (unsigned short val_imarker, su2double val_engine_netthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_GrossThrust (unsigned short val_imarker, su2double val_engine_grossthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_Area (unsigned short val_imarker, su2double val_engine_area) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Mach (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Force (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Power (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_NetThrust (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_GrossThrust (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Area (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Temperature (unsigned short val_imarker, su2double val_actdisk_temp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_TotalTemperature (unsigned short val_imarker, su2double val_actdisk_totaltemp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Temperature (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_TotalTemperature (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Temperature (unsigned short val_imarker, su2double val_actdisk_temp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_TotalTemperature (unsigned short val_imarker, su2double val_actdisk_totaltemp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Temperature (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_TotalTemperature (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_MassFlow (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_MassFlow (unsigned short val_imarker, su2double val_actdisk_massflow) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_MassFlow (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_MassFlow (unsigned short val_imarker, su2double val_actdisk_massflow) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Pressure (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_TotalPressure (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_DeltaPress (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_DeltaTemp (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_TotalPressRatio (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_TotalTempRatio (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_StaticPressRatio (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_StaticTempRatio (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_NetThrust (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_BCThrust (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_BCThrust_Old (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_GrossThrust (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Area (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_ReverseMassFlow (unsigned short val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_RamDrag (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Force (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Power (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Pressure (unsigned short val_imarker, su2double val_actdisk_pressure) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_TotalPressure (unsigned short val_imarker, su2double val_actdisk_totalpressure) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_DeltaPress (unsigned short val_imarker, su2double val_actdisk_deltapress) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Power (unsigned short val_imarker, su2double val_actdisk_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_MassFlow (unsigned short val_imarker, su2double val_actdisk_massflow) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Mach (unsigned short val_imarker, su2double val_actdisk_mach) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Force (unsigned short val_imarker, su2double val_actdisk_force) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_DC60 (unsigned short val_imarker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_MassFlow (unsigned short val_imarker, su2double val_surface_massflow) |
| Set the massflow at the surface. More... | |
| void | SetSurface_Mach (unsigned short val_imarker, su2double val_surface_mach) |
| Set the mach number at the surface. More... | |
| void | SetSurface_Temperature (unsigned short val_imarker, su2double val_surface_temperature) |
| Set the temperature at the surface. More... | |
| void | SetSurface_Pressure (unsigned short val_imarker, su2double val_surface_pressure) |
| Set the pressure at the surface. More... | |
| void | SetSurface_Density (unsigned short val_imarker, su2double val_surface_density) |
| Set the density at the surface. More... | |
| void | SetSurface_Enthalpy (unsigned short val_imarker, su2double val_surface_enthalpy) |
| Set the enthalpy at the surface. More... | |
| void | SetSurface_NormalVelocity (unsigned short val_imarker, su2double val_surface_normalvelocity) |
| Set the normal velocity at the surface. More... | |
| void | SetSurface_Uniformity (unsigned short val_imarker, su2double val_surface_streamwiseuniformity) |
| Set the streamwise flow uniformity at the surface. More... | |
| void | SetSurface_SecondaryStrength (unsigned short val_imarker, su2double val_surface_secondarystrength) |
| Set the secondary flow strength at the surface. More... | |
| void | SetSurface_SecondOverUniform (unsigned short val_imarker, su2double val_surface_secondaryoverstream) |
| Set the relative secondary flow strength at the surface. More... | |
| void | SetSurface_MomentumDistortion (unsigned short val_imarker, su2double val_surface_momentumdistortion) |
| Set the momentum distortion at the surface. More... | |
| void | SetSurface_TotalTemperature (unsigned short val_imarker, su2double val_surface_totaltemperature) |
| Set the total temperature at the surface. More... | |
| void | SetSurface_TotalPressure (unsigned short val_imarker, su2double val_surface_totalpressure) |
| Set the total pressure at the surface. More... | |
| void | SetSurface_PressureDrop (unsigned short val_imarker, su2double val_surface_pressuredrop) |
| Set the pressure drop between two surfaces. More... | |
| void | SetSurface_IDC (unsigned short val_imarker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_IDC_Mach (unsigned short val_imarker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_IDR (unsigned short val_imarker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_DeltaTemp (unsigned short val_imarker, su2double val_actdisk_deltatemp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_TotalPressRatio (unsigned short val_imarker, su2double val_actdisk_pressratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_TotalTempRatio (unsigned short val_imarker, su2double val_actdisk_tempratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_StaticPressRatio (unsigned short val_imarker, su2double val_actdisk_pressratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_StaticTempRatio (unsigned short val_imarker, su2double val_actdisk_tempratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_NetThrust (unsigned short val_imarker, su2double val_actdisk_netthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust (string val_marker, su2double val_actdisk_bcthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust (unsigned short val_imarker, su2double val_actdisk_bcthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust_Old (string val_marker, su2double val_actdisk_bcthrust_old) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust_Old (unsigned short val_imarker, su2double val_actdisk_bcthrust_old) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_GrossThrust (unsigned short val_imarker, su2double val_actdisk_grossthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Area (unsigned short val_imarker, su2double val_actdisk_area) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_ReverseMassFlow (unsigned short val_imarker, su2double val_actdisk_area) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_RamDrag (unsigned short val_imarker, su2double val_actdisk_ramdrag) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Force (unsigned short val_imarker, su2double val_actdisk_force) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Power (unsigned short val_imarker, su2double val_actdisk_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Power (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_MassFlow (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Mach (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Force (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_DC60 (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_MassFlow (unsigned short val_imarker) |
| Get the massflow at an outlet boundary. More... | |
| su2double | GetSurface_Mach (unsigned short val_imarker) |
| Get the mach number at an outlet boundary. More... | |
| su2double | GetSurface_Temperature (unsigned short val_imarker) |
| Get the temperature at an outlet boundary. More... | |
| su2double | GetSurface_Pressure (unsigned short val_imarker) |
| Get the pressure at an outlet boundary. More... | |
| su2double | GetSurface_Density (unsigned short val_imarker) |
| Get the density at an outlet boundary. More... | |
| su2double | GetSurface_Enthalpy (unsigned short val_imarker) |
| Get the enthalpy at an outlet boundary. More... | |
| su2double | GetSurface_NormalVelocity (unsigned short val_imarker) |
| Get the normal velocity at an outlet boundary. More... | |
| su2double | GetSurface_Uniformity (unsigned short val_imarker) |
| Get the streamwise flow uniformity at the surface. More... | |
| su2double | GetSurface_SecondaryStrength (unsigned short val_imarker) |
| Get the secondary flow strength at the surface. More... | |
| su2double | GetSurface_SecondOverUniform (unsigned short val_imarker) |
| Get the relative secondary flow strength at the surface. More... | |
| su2double | GetSurface_MomentumDistortion (unsigned short val_imarker) |
| Get the momentum distortion at the surface. More... | |
| su2double | GetSurface_TotalTemperature (unsigned short val_imarker) |
| Get the total temperature at an outlet boundary. More... | |
| su2double | GetSurface_TotalPressure (unsigned short val_imarker) |
| Get the total pressure at an outlet boundary. More... | |
| su2double | GetSurface_PressureDrop (unsigned short val_imarker) |
| Get the pressure drop between two surfaces. More... | |
| su2double | GetSurface_IDC (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_IDC_Mach (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_IDR (unsigned short val_imarker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Pressure (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_TotalPressure (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_GrossThrust (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Force (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Power (string val_marker) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Pressure (unsigned short val_imarker, su2double val_actdisk_pressure) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_TotalPressure (unsigned short val_imarker, su2double val_actdisk_totalpressure) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_GrossThrust (unsigned short val_imarker, su2double val_actdisk_grossthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Force (unsigned short val_imarker, su2double val_actdisk_force) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Power (unsigned short val_imarker, su2double val_actdisk_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetDispl_Value (string val_index) |
| Get the displacement value at an displacement boundary. More... | |
| su2double | GetLoad_Value (string val_index) |
| Get the force value at an load boundary. More... | |
| su2double | GetDamper_Constant (string val_index) |
| Get the constant value at a damper boundary. More... | |
| su2double | GetLoad_Dir_Value (string val_index) |
| Get the force value at a load boundary defined in cartesian coordinates. More... | |
| su2double | GetLoad_Dir_Multiplier (string val_index) |
| Get the force multiplier at a load boundary in cartesian coordinates. More... | |
| su2double | GetDisp_Dir_Value (string val_index) |
| Get the force value at a load boundary defined in cartesian coordinates. More... | |
| su2double | GetDisp_Dir_Multiplier (string val_index) |
| Get the force multiplier at a load boundary in cartesian coordinates. More... | |
| su2double * | GetLoad_Dir (string val_index) |
| Get the force direction at a loaded boundary in cartesian coordinates. More... | |
| su2double * | GetDisp_Dir (string val_index) |
| Get the force direction at a loaded boundary in cartesian coordinates. More... | |
| su2double | GetLoad_Sine_Amplitude (string val_index) |
| Get the amplitude of the sine-wave at a load boundary defined in cartesian coordinates. More... | |
| su2double | GetLoad_Sine_Frequency (string val_index) |
| Get the frequency of the sine-wave at a load boundary in cartesian coordinates. More... | |
| su2double * | GetLoad_Sine_Dir (string val_index) |
| Get the force direction at a sine-wave loaded boundary in cartesian coordinates. More... | |
| su2double | GetFlowLoad_Value (string val_index) |
| Get the force value at an load boundary. More... | |
| su2double | GetCyclic_Pitch (void) |
| Cyclic pitch amplitude for rotor blades. More... | |
| su2double | GetCollective_Pitch (void) |
| Collective pitch setting for rotor blades. More... | |
| string | GetDV_Filename (void) |
| Get name of the arbitrary mesh motion input file. More... | |
| void | SetConfig_Options (unsigned short val_iZone, unsigned short val_nZone) |
| Set the config options. More... | |
| void | SetRunTime_Options (void) |
| Set the config options. More... | |
| void | SetConfig_Parsing (char case_filename[MAX_STRING_SIZE]) |
| Set the config file parsing. More... | |
| bool | SetRunTime_Parsing (char case_filename[MAX_STRING_SIZE]) |
| Set the config file parsing. More... | |
| void | SetPostprocessing (unsigned short val_software, unsigned short val_izone, unsigned short val_nDim) |
| Config file postprocessing. More... | |
| void | SetMarkers (unsigned short val_software) |
| Config file markers processing. More... | |
| void | SetOutput (unsigned short val_software, unsigned short val_izone) |
| Config file output. More... | |
| vector< vector< su2double > > | GetAeroelastic_np1 (unsigned short iMarker) |
| Value of Aeroelastic solution coordinate at time n+1. More... | |
| vector< vector< su2double > > | GetAeroelastic_n (unsigned short iMarker) |
| Value of Aeroelastic solution coordinate at time n. More... | |
| vector< vector< su2double > > | GetAeroelastic_n1 (unsigned short iMarker) |
| Value of Aeroelastic solution coordinate at time n-1. More... | |
| void | SetAeroelastic_np1 (unsigned short iMarker, vector< vector< su2double > > solution) |
| Value of Aeroelastic solution coordinate at time n+1. More... | |
| void | SetAeroelastic_n (void) |
| Value of Aeroelastic solution coordinate at time n from time n+1. More... | |
| void | SetAeroelastic_n1 (void) |
| Value of Aeroelastic solution coordinate at time n-1 from time n. More... | |
| su2double | GetAeroelastic_Flutter_Speed_Index (void) |
| Aeroelastic Flutter Speed Index. More... | |
| su2double | GetAeroelastic_Frequency_Plunge (void) |
| Uncoupled Aeroelastic Frequency Plunge. More... | |
| su2double | GetAeroelastic_Frequency_Pitch (void) |
| Uncoupled Aeroelastic Frequency Pitch. More... | |
| su2double | GetAeroelastic_Airfoil_Mass_Ratio (void) |
| Aeroelastic Airfoil Mass Ratio. More... | |
| su2double | GetAeroelastic_CG_Location (void) |
| Aeroelastic center of gravity location. More... | |
| su2double | GetAeroelastic_Radius_Gyration_Squared (void) |
| Aeroelastic radius of gyration squared. More... | |
| unsigned short | GetAeroelasticIter (void) |
| Aeroelastic solve every x inner iteration. More... | |
| su2double | GetAeroelastic_plunge (unsigned short val_marker) |
| Value of plunging coordinate. More... | |
| su2double | GetAeroelastic_pitch (unsigned short val_marker) |
| Value of pitching coordinate. More... | |
| void | SetAeroelastic_plunge (unsigned short val_marker, su2double val) |
| Value of plunging coordinate. More... | |
| void | SetAeroelastic_pitch (unsigned short val_marker, su2double val) |
| Value of pitching coordinate. More... | |
| bool | GetAeroelastic_Simulation (void) |
| Get information about the aeroelastic simulation. More... | |
| bool | GetWind_Gust (void) |
| Get information about the wind gust. More... | |
| unsigned short | GetGust_Type (void) |
| Get the type of gust to simulate. More... | |
| unsigned short | GetGust_Dir (void) |
| Get the gust direction. More... | |
| su2double | GetGust_WaveLength (void) |
| Value of the gust wavelength. More... | |
| su2double | GetGust_Periods (void) |
| Value of the number of gust periods. More... | |
| su2double | GetGust_Ampl (void) |
| Value of the gust amplitude. More... | |
| su2double | GetGust_Begin_Time (void) |
| Value of the time at which to begin the gust. More... | |
| su2double | GetGust_Begin_Loc (void) |
| Value of the location ath which the gust begins. More... | |
| unsigned short | GetnFFD_Iter (void) |
| Get the number of iterations to evaluate the parametric coordinates. More... | |
| su2double | GetFFD_Tol (void) |
| Get the tolerance of the point inversion algorithm. More... | |
| su2double | GetOpt_RelaxFactor (void) |
| Get the scale factor for the line search. More... | |
| su2double | GetOpt_LineSearch_Bound (void) |
| Get the bound for the line search. More... | |
| void | SetOpt_RelaxFactor (su2double val_scale) |
| Set the scale factor for the line search. More... | |
| long | GetVisualize_CV (void) |
| Get the node number of the CV to visualize. More... | |
| bool | GetFixed_CL_Mode (void) |
| Get information about whether to use fixed CL mode. More... | |
| bool | GetFixed_CM_Mode (void) |
| Get information about whether to use fixed CL mode. More... | |
| bool | GetEval_dOF_dCX (void) |
| Get information about whether to use fixed CL mode. More... | |
| bool | GetDiscard_InFiles (void) |
| Get information about whether to use fixed CL mode. More... | |
| su2double | GetTarget_CL (void) |
| Get the value specified for the target CL. More... | |
| su2double | GetdCL_dAlpha (void) |
| Get the value for the lift curve slope for fixed CL mode. More... | |
| unsigned long | GetUpdate_Alpha (void) |
| Get the value of iterations to re-evaluate the angle of attack. More... | |
| unsigned long | GetIter_dCL_dAlpha (void) |
| Number of iterations to evaluate dCL_dAlpha. More... | |
| su2double | GetdCM_diH (void) |
| Get the value of the damping coefficient for fixed CL mode. More... | |
| unsigned long | GetIter_Fixed_CL (void) |
| Get the value of iterations to re-evaluate the angle of attack. More... | |
| unsigned long | GetIter_Fixed_NetThrust (void) |
| Get the value of iterations to re-evaluate the angle of attack. More... | |
| su2double | GetdNetThrust_dBCThrust (void) |
| Get the value of the damping coefficient for fixed CL mode. More... | |
| unsigned long | GetUpdate_BCThrust (void) |
| Get the value of iterations to re-evaluate the angle of attack. More... | |
| void | SetUpdate_BCThrust_Bool (bool val_update) |
| Set the value of the boolean for updating AoA in fixed lift mode. More... | |
| void | SetUpdate_AoA (bool val_update) |
| Set the value of the boolean for updating AoA in fixed lift mode. More... | |
| bool | GetUpdate_BCThrust_Bool (void) |
| Get information about whether to update the AoA for fixed lift mode. More... | |
| bool | GetUpdate_AoA (void) |
| Get information about whether to update the AoA for fixed lift mode. More... | |
| void | SetNonphysical_Points (unsigned long val_nonphys_points) |
| Set the current number of non-physical nodes in the solution. More... | |
| unsigned long | GetNonphysical_Points (void) |
| Get the current number of non-physical nodes in the solution. More... | |
| void | SetNonphysical_Reconstr (unsigned long val_nonphys_reconstr) |
| Set the current number of non-physical reconstructions for 2nd-order upwinding. More... | |
| unsigned long | GetNonphysical_Reconstr (void) |
| Get the current number of non-physical reconstructions for 2nd-order upwinding. More... | |
| void | SetSpline (vector< su2double > &x, vector< su2double > &y, unsigned long n, su2double yp1, su2double ypn, vector< su2double > &y2) |
| Given arrays x[1..n] and y[1..n] containing a tabulated function, i.e., yi = f(xi), with x1 < x2 < . . . < xN , and given values yp1 and ypn for the first derivative of the interpolating function at points 1 and n, respectively, this routine returns an array y2[1..n] that contains the second derivatives of the interpolating function at the tabulated points xi. If yp1 and/or ypn are equal to 1 × 1030 or larger, the routine is signaled to set the corresponding boundary condition for a natural spline, with zero second derivative on that boundary. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++. More... | |
| su2double | GetSpline (vector< su2double > &xa, vector< su2double > &ya, vector< su2double > &y2a, unsigned long n, su2double x) |
| Given the arrays xa[1..n] and ya[1..n], which tabulate a function (with the xai’s in order), and given the array y2a[1..n], which is the output from spline above, and given a value of x, this routine returns a cubic-spline interpolated value y. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++. More... | |
| void | Tick (double *val_start_time) |
| Start the timer for profiling subroutines. More... | |
| void | Tock (double val_start_time, string val_function_name, int val_group_id) |
| Stop the timer for profiling subroutines and store results. More... | |
| void | SetProfilingCSV (void) |
| Write a CSV file containing the results of the profiling. More... | |
| void | GEMM_Tick (double *val_start_time) |
| Start the timer for profiling subroutines. More... | |
| void | GEMM_Tock (double val_start_time, int M, int N, int K) |
| Stop the timer for the GEMM profiling and store results. More... | |
| void | GEMMProfilingCSV (void) |
| Write a CSV file containing the results of the profiling. More... | |
| void | SetFreeStreamTurboNormal (su2double *turboNormal) |
| Set freestream turbonormal for initializing solution. More... | |
| su2double * | GetFreeStreamTurboNormal (void) |
| Set freestream turbonormal for initializing solution. More... | |
| unsigned short | GetConsole_Output_Verb (void) |
| Get the verbosity level of the console output. More... | |
| unsigned short | GetKind_Average (void) |
| Get the kind of marker analyze marker (area-averaged, mass flux averaged, etc). More... | |
| unsigned short | GetDirectDiff () |
| Get the direct differentation method. More... | |
| bool | GetDiscrete_Adjoint (void) |
| Get the indicator whether we are solving an discrete adjoint problem. More... | |
| bool | CheckFSI_MPI (void) |
| Get the indicator whether we want to benchmark the MPI performance of FSI problems. More... | |
| unsigned short | GetnIterFSI (void) |
| Get the number of fluid subiterations roblems. More... | |
| unsigned short | GetnIterFSI_Ramp (void) |
| Get the number of subiterations while a ramp is applied. More... | |
| su2double | GetAitkenStatRelax (void) |
| Get Aitken's relaxation parameter for static relaxation cases. More... | |
| su2double | GetAitkenDynMaxInit (void) |
| Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration. More... | |
| su2double | GetAitkenDynMinInit (void) |
| Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration. More... | |
| bool | GetDeadLoad (void) |
| Decide whether to apply dead loads to the model. More... | |
| bool | GetPseudoStatic (void) |
| Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures). More... | |
| bool | GetMatchingMesh (void) |
| Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures). More... | |
| bool | GetSteadyRestart (void) |
| Identifies if we want to restart from a steady or an unsteady solution. More... | |
| unsigned short | GetDynamic_Analysis (void) |
| Provides information about the time integration of the structural analysis, and change the write in the output files information about the iteration. More... | |
| su2double | GetDelta_DynTime (void) |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| su2double | GetTotal_DynTime (void) |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| su2double | GetCurrent_DynTime (void) |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| unsigned short | GetiInst (void) |
| Get the current instance. More... | |
| void | SetiInst (unsigned short val_iInst) |
| Set the current instance. More... | |
| bool | GetWrt_Dynamic (void) |
| Get information about writing dynamic structural analysis headers and file extensions. More... | |
| su2double | GetNewmark_beta (void) |
| Get Newmark alpha parameter. More... | |
| su2double | GetNewmark_gamma (void) |
| Get Newmark delta parameter. More... | |
| unsigned short | GetnIntCoeffs (void) |
| Get the number of integration coefficients provided by the user. More... | |
| unsigned short | GetnElasticityMod (void) |
| Get the number of different values for the elasticity modulus. More... | |
| unsigned short | GetnPoissonRatio (void) |
| Get the number of different values for the Poisson ratio. More... | |
| unsigned short | GetnMaterialDensity (void) |
| Get the number of different values for the Material density. More... | |
| su2double | Get_Int_Coeffs (unsigned short val_coeff) |
| Get the integration coefficients for the Generalized Alpha - Newmark integration integration scheme. More... | |
| unsigned short | GetnElectric_Field (void) |
| Get the number of different values for the modulus of the electric field. More... | |
| unsigned short | GetnDim_Electric_Field (void) |
| Get the dimensionality of the electric field. More... | |
| su2double | Get_Electric_Field_Mod (unsigned short val_coeff) |
| Get the values for the electric field modulus. More... | |
| void | Set_Electric_Field_Mod (unsigned short val_coeff, su2double val_el_field) |
| Set the values for the electric field modulus. More... | |
| su2double * | Get_Electric_Field_Dir (void) |
| Get the direction of the electric field in reference configuration. More... | |
| bool | GetRamp_Load (void) |
| Check if the user wants to apply the load as a ramp. More... | |
| su2double | GetRamp_Time (void) |
| Get the maximum time of the ramp. More... | |
| bool | GetRampAndRelease_Load (void) |
| Check if the user wants to apply the load as a ramp. More... | |
| bool | GetSine_Load (void) |
| Check if the user wants to apply the load as a ramp. More... | |
| su2double * | GetLoad_Sine (void) |
| Get the sine load properties. More... | |
| unsigned short | GetDynamic_LoadTransfer (void) |
| Get the kind of load transfer method we want to use for dynamic problems. More... | |
| su2double | GetRefGeom_Penalty (void) |
| Get the penalty weight value for the objective function. More... | |
| su2double | GetTotalDV_Penalty (void) |
| Get the penalty weight value for the objective function. More... | |
| unsigned short | GetPredictorOrder (void) |
| Get the order of the predictor for FSI applications. More... | |
| bool | GetEulerPersson (void) |
| Get boolean for using Persson's shock capturing method in Euler flow DG-FEM. More... | |
| void | SetEulerPersson (bool val_EulerPersson) |
| Set boolean for using Persson's shock capturing method in Euler flow DG-FEM. More... | |
| bool | GetFSI_Simulation (void) |
| Check if the simulation we are running is a FSI simulation. More... | |
| unsigned short | GetnID_DV (void) |
| Get the ID for the FEA region that we want to compute the gradient for using direct differentiation. More... | |
| bool | GetIncrementalLoad (void) |
| Check if we want to apply an incremental load to the nonlinear structural simulation. More... | |
| unsigned long | GetNumberIncrements (void) |
| Get the number of increments for an incremental load. More... | |
| su2double | GetIncLoad_Criteria (unsigned short val_var) |
| Get the value of the criteria for applying incremental loading. More... | |
| unsigned short | GetRelaxation_Method_FSI (void) |
| Get the relaxation method chosen for the simulation. More... | |
| unsigned short | GetRiemann_Solver_FEM (void) |
| Get the kind of Riemann solver for the DG method (FEM flow solver). More... | |
| su2double | GetQuadrature_Factor_Straight (void) |
| Get the factor applied during quadrature of straight elements. More... | |
| su2double | GetQuadrature_Factor_Curved (void) |
| Get the factor applied during quadrature of curved elements. More... | |
| su2double | GetQuadrature_Factor_Time_ADER_DG (void) |
| Get the factor applied during time quadrature for ADER-DG. More... | |
| su2double | GetTheta_Interior_Penalty_DGFEM (void) |
| Function to make available the multiplication factor theta of the symmetrizing terms in the DG discretization of the viscous terms. More... | |
| unsigned short | GetSizeMatMulPadding (void) |
| Function to make available the matrix size in vectorization in order to optimize the gemm performance. More... | |
| bool | GetCompute_Entropy (void) |
| Function to make available whether or not the entropy must be computed. More... | |
| bool | GetUse_Lumped_MassMatrix_DGFEM (void) |
| Function to make available whether or not the lumped mass matrix must be used for steady computations. More... | |
| bool | GetJacobian_Spatial_Discretization_Only (void) |
| Function to make available whether or not only the exact Jacobian of the spatial discretization must be computed. More... | |
| unsigned short | GetKindInterpolation (void) |
| Get the interpolation method used for matching between zones. More... | |
| bool | GetConservativeInterpolation (void) |
| Get option of whether to use conservative interpolation between zones. More... | |
| unsigned short | GetKindRadialBasisFunction (void) |
| Get the basis function to use for radial basis function interpolation for FSI. More... | |
| bool | GetRadialBasisFunctionPolynomialOption (void) |
| Get option of whether to use polynomial terms in Radial Basis Function interpolation. More... | |
| su2double | GetRadialBasisFunctionParameter (void) |
| Get the basis function radius to use for radial basis function interpolation for FSI. More... | |
| bool | GetWall_Functions (void) |
| Get information about whether to use wall functions. More... | |
| bool | GetAD_Mode (void) |
| Get the AD support. More... | |
| void | SetMax_Vel2 (su2double val_max_vel2) |
| Set the maximum velocity^2 in the domain for the incompressible preconditioner. More... | |
| su2double | GetMax_Vel2 (void) |
| Get the maximum velocity^2 in the domain for the incompressible preconditioner. More... | |
| void | SetRestart_Bandwidth_Agg (su2double val_restart_bandwidth_sum) |
| Set the sum of the bandwidth for writing binary restarts (to be averaged later). More... | |
| su2double | GetRestart_Bandwidth_Agg (void) |
| Set the sum of the bandwidth for writing binary restarts (to be averaged later). More... | |
| unsigned long | GetWrt_Surf_Freq_DualTime (void) |
| Get the frequency for writing the surface solution file in Dual Time. More... | |
| unsigned short | GetKind_HybridRANSLES (void) |
| Get the Kind of Hybrid RANS/LES. More... | |
| unsigned short | GetKind_RoeLowDiss (void) |
| Get the Kind of Roe Low Dissipation Scheme for Unsteady flows. More... | |
| su2double | GetConst_DES (void) |
| Get the DES Constant. More... | |
| bool | GetQCR (void) |
| Get QCR (SA-QCR2000). More... | |
| bool | GetAD_Preaccumulation (void) |
| Get if AD preaccumulation should be performed. More... | |
| bool | GetWeakly_Coupled_Heat (void) |
| Get the heat equation. More... | |
| bool | GetIntegrated_HeatFlux (void) |
| Check if values passed to the BC_HeatFlux-Routine are already integrated. More... | |
| ofstream * | GetHistFile (void) |
| Retrieve the ofstream of the history file for the current zone. More... | |
| void | SetHistFile (ofstream *HistFile) |
| Set the ofstream of the history file for the current zone. More... | |
| bool | GetCompute_Average (void) |
| Get Compute Average. More... | |
Static Public Member Functions | |
| static unsigned short | GetnZone (string val_mesh_filename, unsigned short val_format, CConfig *config) |
| Gets the number of zones in the mesh file. More... | |
| static unsigned short | GetnDim (string val_mesh_filename, unsigned short val_format) |
| Gets the number of dimensions in the mesh file. More... | |
| static bool | GetPeriodic (string val_mesh_filename, unsigned short val_format, CConfig *config) |
| Determine whether there are periodic BCs in the grid. More... | |
Public Attributes | |
| vector< string > | fields |
| Tags for the different fields in a restart file. More... | |
Main class for defining the problem; basically this class reads the configuration file, and stores all the information.
Definition at line 71 of file config_structure.hpp.
| CConfig::CConfig | ( | char | case_filename[MAX_STRING_SIZE], |
| unsigned short | val_software, | ||
| unsigned short | val_iZone, | ||
| unsigned short | val_nZone, | ||
| unsigned short | val_nDim, | ||
| unsigned short | verb_level | ||
| ) |
Constructor of the class which reads the input file.
Definition at line 60 of file config_structure.cpp.
| CConfig::CConfig | ( | char | case_filename[MAX_STRING_SIZE], |
| unsigned short | val_software | ||
| ) |
Constructor of the class which reads the input file.
Definition at line 94 of file config_structure.cpp.
| CConfig::CConfig | ( | char | case_filename[MAX_STRING_SIZE], |
| CConfig * | config | ||
| ) |
Constructor of the class which reads the input file.
Definition at line 123 of file config_structure.cpp.
| CConfig::~CConfig | ( | void | ) |
Destructor of the class.
Definition at line 6585 of file config_structure.cpp.
|
inline |
Decide whether it's necessary to add the cross term for adjoint FSI.
TRUE if it's necessary to add the cross term, FALSE otherwise. Definition at line 410 of file config_structure.inl.
| bool CConfig::CheckFSI_MPI | ( | void | ) |
Get the indicator whether we want to benchmark the MPI performance of FSI problems.
| void CConfig::GEMM_Tick | ( | double * | val_start_time | ) |
Start the timer for profiling subroutines.
| [in] | val_start_time | - the value of the start time. |
Definition at line 8676 of file config_structure.cpp.
| void CConfig::GEMM_Tock | ( | double | val_start_time, |
| int | M, | ||
| int | N, | ||
| int | K | ||
| ) |
Stop the timer for the GEMM profiling and store results.
| [in] | val_start_time | - The value of the start time. |
| [in] | M,N,K | - Matrix size of the GEMM call. |
Definition at line 8692 of file config_structure.cpp.
| void CConfig::GEMMProfilingCSV | ( | void | ) |
Write a CSV file containing the results of the profiling.
Definition at line 8741 of file config_structure.cpp.
|
inline |
Get the alpha (convective) coefficients for the Runge-Kutta integration scheme.
| [in] | val_step | - Index of the step. |
Definition at line 801 of file config_structure.inl.
|
inline |
Get the direction of the electric field in reference configuration.
| [in] | val_coeff | - Index of the coefficient. |
Definition at line 1843 of file config_structure.inl.
|
inline |
Get the values for the electric field modulus.
| [in] | val_coeff | - Index of the coefficient. |
Definition at line 1839 of file config_structure.inl.
|
inline |
Get the integration coefficients for the Generalized Alpha - Newmark integration integration scheme.
| [in] | val_coeff | - Index of the coefficient. |
Definition at line 1833 of file config_structure.inl.
|
inline |
number span-wise sections to compute 3D BC and performance for turbomachinery specified by the user.
Definition at line 1244 of file config_structure.inl.
|
inline |
Get the value of the critical pressure.
Definition at line 870 of file config_structure.inl.
| su2double CConfig::GetActDisk_Area | ( | string | val_marker | ) |
Get the tip radius of th actuator disk.
Definition at line 7503 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 230 of file config_structure.inl.
| su2double CConfig::GetActDisk_BCThrust | ( | string | val_marker | ) |
Get the origin of the actuator disk.
Definition at line 7471 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 224 of file config_structure.inl.
| su2double CConfig::GetActDisk_BCThrust_Old | ( | string | val_marker | ) |
Get the origin of the actuator disk.
Definition at line 7479 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 226 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 166 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 168 of file config_structure.inl.
|
inline |
Actuator disk defined with a double surface.
TRUE if the elements must be divided; otherwise FALSE. Definition at line 1519 of file config_structure.inl.
| su2double CConfig::GetActDisk_Force | ( | string | val_marker | ) |
Get the origin of the actuator disk.
Definition at line 7463 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 184 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 228 of file config_structure.inl.
|
inline |
Get the format of the output solution.
Definition at line 1437 of file config_structure.inl.
| su2double CConfig::GetActDisk_Mach | ( | string | val_marker | ) |
Get the origin of the actuator disk.
Definition at line 7455 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 182 of file config_structure.inl.
| su2double CConfig::GetActDisk_MassFlow | ( | string | val_marker | ) |
Get the origin of the actuator disk.
Definition at line 7447 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 180 of file config_structure.inl.
| su2double CConfig::GetActDisk_NetThrust | ( | string | val_marker | ) |
Get the origin of the actuator disk.
Definition at line 7431 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 222 of file config_structure.inl.
| su2double CConfig::GetActDisk_Omega | ( | string | val_marker, |
| unsigned short | val_index | ||
| ) |
Get the rev / min of the actuator disk.
Definition at line 7535 of file config_structure.cpp.
| su2double CConfig::GetActDisk_Power | ( | string | val_marker | ) |
Get the origin of the actuator disk.
Definition at line 7439 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 178 of file config_structure.inl.
| su2double CConfig::GetActDisk_PressJump | ( | string | val_marker, |
| unsigned short | val_index | ||
| ) |
Get the thrust corffient of the actuator disk.
Definition at line 7519 of file config_structure.cpp.
| su2double CConfig::GetActDisk_ReverseMassFlow | ( | string | val_marker | ) |
Get the tip radius of th actuator disk.
Definition at line 7511 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 232 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 174 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 176 of file config_structure.inl.
|
inline |
Actuator disk defined with a double surface.
TRUE if the elements must be divided; otherwise FALSE. Definition at line 1523 of file config_structure.inl.
| su2double CConfig::GetActDisk_TempJump | ( | string | val_marker, |
| unsigned short | val_index | ||
| ) |
Get the thrust corffient of the actuator disk.
Definition at line 7527 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 170 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 172 of file config_structure.inl.
| su2double CConfig::GetActDiskInlet_Force | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8240 of file config_structure.cpp.
| su2double CConfig::GetActDiskInlet_MassFlow | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8317 of file config_structure.cpp.
| su2double CConfig::GetActDiskInlet_Power | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8247 of file config_structure.cpp.
| su2double CConfig::GetActDiskInlet_Pressure | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8219 of file config_structure.cpp.
| su2double CConfig::GetActDiskInlet_RamDrag | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8233 of file config_structure.cpp.
| su2double CConfig::GetActDiskInlet_Temperature | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8289 of file config_structure.cpp.
| su2double CConfig::GetActDiskInlet_TotalPressure | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8226 of file config_structure.cpp.
| su2double CConfig::GetActDiskInlet_TotalTemperature | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8296 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_Force | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8275 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_GrossThrust | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8268 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_MassFlow | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8324 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_Power | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8282 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_Pressure | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8254 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_Temperature | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8303 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_TotalPressure | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8261 of file config_structure.cpp.
| su2double CConfig::GetActDiskOutlet_TotalTemperature | ( | string | val_marker | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8310 of file config_structure.cpp.
|
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Get the AD support.
Definition at line 1935 of file config_structure.inl.
|
inline |
Get if AD preaccumulation should be performed.
Definition at line 1937 of file config_structure.inl.
|
inline |
Get information about there is a smoothing of the grid coordinates.
TRUE if there is smoothing of the grid coordinates; otherwise FALSE. Definition at line 1583 of file config_structure.inl.
| bool CConfig::GetAdiabaticWall | ( | void | ) |
Get information about the adibatic wall condition.
TRUE if it is a adiabatic wall condition; otherwise FALSE.
|
inline |
Get the name of the file with the adjoint variables.
Definition at line 1477 of file config_structure.inl.
|
inline |
Get the limit value for the adjoint variables.
Definition at line 336 of file config_structure.inl.
|
inline |
Get the value of sharp edge limiter.
Definition at line 609 of file config_structure.inl.
|
inline |
Get the name of the file with the adjoint structure variables.
Definition at line 1459 of file config_structure.inl.
|
inline |
Get the name of the file with the adjoint structure variables.
Definition at line 1461 of file config_structure.inl.
|
inline |
Get min error of the linear solver for the implicit formulation.
Definition at line 1026 of file config_structure.inl.
|
inline |
Get max number of iterations of the linear solver for the implicit formulation.
Definition at line 1030 of file config_structure.inl.
|
inline |
Aeroelastic Airfoil Mass Ratio.
Definition at line 1709 of file config_structure.inl.
|
inline |
Aeroelastic center of gravity location.
Definition at line 1711 of file config_structure.inl.
|
inline |
Aeroelastic Flutter Speed Index.
Definition at line 1703 of file config_structure.inl.
|
inline |
Uncoupled Aeroelastic Frequency Pitch.
Definition at line 1707 of file config_structure.inl.
|
inline |
Uncoupled Aeroelastic Frequency Plunge.
Definition at line 1705 of file config_structure.inl.
|
inline |
Value of Aeroelastic solution coordinate at time n.
Definition at line 1681 of file config_structure.inl.
|
inline |
Value of Aeroelastic solution coordinate at time n-1.
Definition at line 1683 of file config_structure.inl.
|
inline |
Value of Aeroelastic solution coordinate at time n+1.
Definition at line 1679 of file config_structure.inl.
|
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Value of pitching coordinate.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 1689 of file config_structure.inl.
|
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Value of plunging coordinate.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 1687 of file config_structure.inl.
|
inline |
Aeroelastic radius of gyration squared.
Definition at line 1713 of file config_structure.inl.
|
inline |
Get information about the aeroelastic simulation.
TRUE if it is an aeroelastic case; otherwise FALSE. Definition at line 1719 of file config_structure.inl.
|
inline |
Aeroelastic solve every x inner iteration.
Definition at line 1715 of file config_structure.inl.
|
inline |
Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration.
Definition at line 1801 of file config_structure.inl.
|
inline |
Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration.
Definition at line 1803 of file config_structure.inl.
|
inline |
Get Aitken's relaxation parameter for static relaxation cases.
Definition at line 1799 of file config_structure.inl.
|
inline |
Get Information about if there is an analytical definition of the surface for doing the grid adaptation.
Definition at line 346 of file config_structure.inl.
|
inline |
Get the angle of attack of the body. This is the angle between a reference line on a lifting body (often the chord line of an airfoil) and the vector representing the relative motion between the lifting body and the fluid through which it is moving.
Definition at line 707 of file config_structure.inl.
|
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Get the off set angle of attack of the body. The solution and the geometry file are able to modifity the angle of attack in the config file.
Definition at line 721 of file config_structure.inl.
|
inline |
Get the functional sensitivity with respect to changes in the angle of attack.
Definition at line 725 of file config_structure.inl.
|
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Get the angle of sideslip of the body. It relates to the rotation of the aircraft centerline from the relative wind.
Definition at line 719 of file config_structure.inl.
|
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Get the off set sideslip angle of the body. The solution and the geometry file are able to modifity the angle of attack in the config file.
Definition at line 723 of file config_structure.inl.
| su2double CConfig::GetArrheniusCoeff | ( | unsigned short | iReaction | ) |
Provides the number of chemical reactions in the chemistry model.
| su2double CConfig::GetArrheniusEta | ( | unsigned short | iReaction | ) |
Provides the number of chemical reactions in the chemistry model.
| su2double CConfig::GetArrheniusTheta | ( | unsigned short | iReaction | ) |
Provides the number of chemical reactions in the chemistry model.
|
inline |
Get mach limit for average massflow-based procedure .
Definition at line 1208 of file config_structure.inl.
|
inline |
Get information about the axisymmetric frame.
TRUE if there is a rotational frame; otherwise FALSE. Definition at line 1581 of file config_structure.inl.
|
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Get the epsilon^2 multiplier for Beta in the incompressible preconditioner.
Definition at line 444 of file config_structure.inl.
| su2double CConfig::GetBlottnerCoeff | ( | unsigned short | val_Species, |
| unsigned short | val_Coeff | ||
| ) |
Get the coefficients of the Blottner viscosity model.
| [in] | val_Species | - Index of the species |
| [in] | val_Coeff | - Index of the coefficient (As, Bs, Cs) |
|
inline |
Get information about the body force.
TRUE if it uses a body force; otherwise FALSE. Definition at line 1593 of file config_structure.inl.
|
inline |
Get a pointer to the body force vector.
Definition at line 1595 of file config_structure.inl.
|
inline |
Verify if there is any Giles Boundary Condition option specified from config file.
Definition at line 1230 of file config_structure.inl.
|
inline |
Verify if there is mixing plane interface specified from config file.
Definition at line 1216 of file config_structure.inl.
|
inline |
Verify if there is any Riemann Boundary Condition option specified from config file.
Definition at line 1232 of file config_structure.inl.
|
inline |
Verify if there is mixing plane interface specified from config file.
Definition at line 1222 of file config_structure.inl.
|
inline |
Verify if there is Turbomachinery performance option specified from config file.
Definition at line 1218 of file config_structure.inl.
|
inline |
Verify if there are zone specific solvers entered in the config file.
Definition at line 1220 of file config_structure.inl.
|
inline |
Get the name of the file with the forces breakdown of the problem.
Definition at line 1443 of file config_structure.inl.
|
inline |
Get the buffet sensor sharpness coefficient.
Definition at line 745 of file config_structure.inl.
|
inline |
Get the buffet sensor offset parameter.
Definition at line 747 of file config_structure.inl.
|
inline |
Provides the buffet monitoring information.
TRUE then the code will compute the buffet sensor. Definition at line 743 of file config_structure.inl.
|
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Get the value of the bulk modulus.
Definition at line 442 of file config_structure.inl.
|
inline |
Get the number of iterations that are considered in the Cauchy convergence criteria.
Definition at line 1499 of file config_structure.inl.
|
inline |
Get the value of convergence criteria for the Cauchy method in the direct, adjoint or linearized problem.
Definition at line 1503 of file config_structure.inl.
|
inline |
Get functional that is going to be used to evaluate the adjoint flow convergence.
Definition at line 1497 of file config_structure.inl.
|
inline |
Get functional that is going to be used to evaluate the flow convergence.
Definition at line 1495 of file config_structure.inl.
|
inline |
Get the Courant Friedrich Levi number for each grid.
| [in] | val_mesh | - Index of the mesh were the CFL is applied. |
Definition at line 755 of file config_structure.inl.
|
inline |
Get the values of the CFL adapation.
Definition at line 44 of file config_structure.inl.
|
inline |
Get the values of the CFL adapation.
Definition at line 42 of file config_structure.inl.
|
inline |
Get the Courant Friedrich Levi number for solid solvers.
| [in] | val_mesh | - Index of the mesh were the CFL is applied. |
Definition at line 757 of file config_structure.inl.
|
inline |
Get CFL reduction factor for adjoint turbulence model.
Definition at line 1032 of file config_structure.inl.
|
inline |
Value of the CFL reduction in LevelSet problems.
Definition at line 1575 of file config_structure.inl.
| su2double** CConfig::GetCharElTemp | ( | void | ) |
Provides the characteristic electronic temperature for calculating e_el.
|
inline |
Get the charge coefficient that is used in the poissonal potential simulation.
Definition at line 603 of file config_structure.inl.
| su2double CConfig::GetCharVibTemp | ( | unsigned short | iSpecies | ) |
Provides the characteristic vibrational temperature for calculating e_vib.
| su2double* CConfig::GetCharVibTemp | ( | void | ) |
Provides the characteristic vibrational temperature for calculating e_vib.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1569 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1571 of file config_structure.inl.
|
inline |
Get the coefficients of the objective defined by the chain rule with primitive variables.
Definition at line 1280 of file config_structure.inl.
|
inline |
Collective pitch setting for rotor blades.
Definition at line 1643 of file config_structure.inl.
| bool CConfig::GetComboObj | ( | void | ) |
Get the flag indicating whether to comput a combined objective.
|
inline |
Get Compute Average.
Definition at line 1961 of file config_structure.inl.
|
inline |
Function to make available whether or not the entropy must be computed.
Definition at line 1925 of file config_structure.inl.
|
inline |
Get the value of the reference conductivity for non-dimensionalization.
Definition at line 526 of file config_structure.inl.
|
inline |
Get option of whether to use conservative interpolation between zones.
Definition at line 1883 of file config_structure.inl.
|
inline |
Get the verbosity level of the console output.
Definition at line 1791 of file config_structure.inl.
|
inline |
Get the DES Constant.
Definition at line 1957 of file config_structure.inl.
| unsigned short CConfig::GetContainerPosition | ( | unsigned short | val_eqsystem | ) |
Provides the index of the solution in the container.
| [in] | val_eqsystem | - Equation that is being solved. |
Definition at line 7208 of file config_structure.cpp.
|
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Determines if problem is adjoint.
Definition at line 290 of file config_structure.inl.
|
inline |
Get the name of the file with the convergence history of the problem.
Definition at line 1439 of file config_structure.inl.
|
inline |
Get the name of the file with the convergence history of the problem for FSI applications.
Definition at line 1441 of file config_structure.inl.
|
inline |
Obtain the kind of convergence criteria to establish the convergence of the CFD code.
Definition at line 749 of file config_structure.inl.
|
inline |
Get the coordinates of the FFD corner points.
| [in] | val_ffd | - Index of the FFD box. |
| [in] | val_coord | - Index of the coordinate that we want to read. |
Definition at line 767 of file config_structure.inl.
|
inline |
Value of the maximum objective function for FEM elasticity adjoint (log10 scale).
Definition at line 1905 of file config_structure.inl.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 1819 of file config_structure.inl.
|
inline |
If we are performing an unsteady simulation, this is the value of current time.
Definition at line 1511 of file config_structure.inl.
|
inline |
Cyclic pitch amplitude for rotor blades.
Definition at line 1641 of file config_structure.inl.
|
inline |
Value of the damping factor for the correction prolongation.
Definition at line 1539 of file config_structure.inl.
|
inline |
Value of the damping factor for the engine exhaust inlet bc.
Definition at line 1535 of file config_structure.inl.
|
inline |
Value of the damping factor for the engine inlet bc.
Definition at line 1533 of file config_structure.inl.
|
inline |
Value of the damping factor for the residual restriction.
Definition at line 1537 of file config_structure.inl.
| su2double CConfig::GetDamper_Constant | ( | string | val_index | ) |
Get the constant value at a damper boundary.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8345 of file config_structure.cpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1545 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1565 of file config_structure.inl.
|
inline |
Get the value for the lift curve slope for fixed CL mode.
Definition at line 1759 of file config_structure.inl.
|
inline |
Get the value of the damping coefficient for fixed CL mode.
Definition at line 1761 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1547 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1549 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1551 of file config_structure.inl.
|
inline |
Decide whether to apply DE effects to the model.
TRUE if the DE effects are to be applied, FALSE otherwise. Definition at line 366 of file config_structure.inl.
| bool CConfig::GetDE_Predicted | ( | void | ) |
Decide whether to predict the DE effects for the next time step.
TRUE if the DE effects are to be applied, FALSE otherwise.
|
inline |
Decide whether to apply dead loads to the model.
TRUE if the dead loads are to be applied, FALSE otherwise. Definition at line 1805 of file config_structure.inl.
| bool CConfig::GetDebugMode | ( | void | ) |
Get information about the axisymmetric frame.
TRUE if there is a rotational frame; otherwise FALSE.
|
inline |
Get factor to multiply smallest volume for deform tolerance.
Definition at line 1042 of file config_structure.inl.
|
inline |
Get Young's modulus for deformation (constant stiffness deformation)
Definition at line 1046 of file config_structure.inl.
|
inline |
Get limit for the volumetric deformation.
Definition at line 1044 of file config_structure.inl.
|
inline |
Get min error of the linear solver for the implicit formulation.
Definition at line 992 of file config_structure.inl.
|
inline |
Get max number of iterations of the linear solver for the implicit formulation.
Definition at line 996 of file config_structure.inl.
|
inline |
Get information about writing grid deformation residuals to the console.
TRUE means that grid deformation residuals will be written to the console. Definition at line 1038 of file config_structure.inl.
|
inline |
Get Poisson's ratio for deformation (constant stiffness deformation) .
Definition at line 1048 of file config_structure.inl.
|
inline |
Get the type of stiffness to impose for FEA mesh deformation.
Definition at line 1050 of file config_structure.inl.
|
inline |
Get factor to multiply smallest volume for deform tolerance.
Definition at line 1040 of file config_structure.inl.
|
inline |
Get the degree of the FFD corner points.
| [in] | val_ffd | - Index of the FFD box. |
| [in] | val_degree | - Index (I,J,K) to obtain the degree. |
Definition at line 769 of file config_structure.inl.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 1815 of file config_structure.inl.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 1509 of file config_structure.inl.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 1505 of file config_structure.inl.
|
inline |
Get the value of the frestream temperature.
Definition at line 490 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream density.
Definition at line 542 of file config_structure.inl.
|
inline |
Get the value of the reference density for non-dimensionalization.
Definition at line 516 of file config_structure.inl.
|
inline |
Get the value of the solid density.
Definition at line 492 of file config_structure.inl.
|
inline |
Obtain the kind of design variable.
| [in] | val_dv | - Number of the design variable that we want to read. |
Definition at line 737 of file config_structure.inl.
|
inline |
Get the direct differentation method.
Definition at line 1909 of file config_structure.inl.
| bool CConfig::GetDirichlet_Boundary | ( | string | val_index | ) |
Get whether this is a Dirichlet or a Neumann boundary.
| [in] | val_index | - Index corresponding to the Dirichlet boundary. |
Definition at line 7610 of file config_structure.cpp.
| su2double CConfig::GetDirichlet_Value | ( | string | val_index | ) |
Get the fixed value at the Dirichlet boundary.
| [in] | val_index | - Index corresponding to the Dirichlet boundary. |
Definition at line 7603 of file config_structure.cpp.
|
inline |
Get information about whether to use fixed CL mode.
TRUE if fixed CL mode is active; otherwise FALSE. Definition at line 1755 of file config_structure.inl.
|
inline |
Get the indicator whether we are solving an discrete adjoint problem.
Definition at line 1911 of file config_structure.inl.
| su2double * CConfig::GetDisp_Dir | ( | string | val_index | ) |
Get the force direction at a loaded boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8387 of file config_structure.cpp.
| su2double CConfig::GetDisp_Dir_Multiplier | ( | string | val_index | ) |
Get the force multiplier at a load boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8373 of file config_structure.cpp.
| su2double CConfig::GetDisp_Dir_Value | ( | string | val_index | ) |
Get the force value at a load boundary defined in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8366 of file config_structure.cpp.
| su2double CConfig::GetDispl_Value | ( | string | val_index | ) |
Get the displacement value at an displacement boundary.
| [in] | val_index | - Index corresponding to the displacement boundary. |
Definition at line 8331 of file config_structure.cpp.
| su2double* CConfig::GetDissociationPot | ( | void | ) |
Dissociation potential of species.
|
inline |
Get the the coordinates where of the box where a subsonic region is imposed.
Definition at line 344 of file config_structure.inl.
|
inline |
Get the value of the damping coefficient for fixed CL mode.
Definition at line 1781 of file config_structure.inl.
|
inline |
Get the volume of the whole domain using the fine grid, this value is common for all the grids in the multigrid method.
Definition at line 424 of file config_structure.inl.
|
inline |
Get the power of the dual volume in the grid adaptation sensor.
Definition at line 350 of file config_structure.inl.
|
inline |
Get the kind of design variable for FEA.
Definition at line 376 of file config_structure.inl.
|
inline |
Get name of the arbitrary mesh motion input file.
Definition at line 1645 of file config_structure.inl.
|
inline |
Value of the design variable step, we use this value in design problems.
| [in] | val_dv | - Number of the design variable that we want to read. |
| [in] | val_value | - Value of the design variable that we want to read. |
Definition at line 1525 of file config_structure.inl.
|
inline |
Get the number of internal iterations for the Newton-Raphson Method in nonlinear structural applications.
Definition at line 318 of file config_structure.inl.
|
inline |
Get the restart iteration number for dynamic structural simulations.
Definition at line 328 of file config_structure.inl.
|
inline |
Provides information about the time integration of the structural analysis, and change the write in the output files information about the iteration.
Definition at line 1813 of file config_structure.inl.
|
inline |
Get the kind of load transfer method we want to use for dynamic problems.
Definition at line 1907 of file config_structure.inl.
|
inline |
Get the integration limits for the equivalent area computation.
| [in] | index | - 0 means x_min, and 1 means x_max. |
Definition at line 332 of file config_structure.inl.
|
inline |
Get the integration limits for the equivalent area computation.
| [in] | index | - 0 means x_min, and 1 means x_max. |
Definition at line 334 of file config_structure.inl.
|
inline |
Formulation for 2D elasticity (plane stress - strain)
Definition at line 390 of file config_structure.inl.
|
inline |
Get the Young's modulus of elasticity.
Definition at line 364 of file config_structure.inl.
| su2double** CConfig::GetElDegeneracy | ( | void | ) |
Provides the degeneracy of electron states for calculating e_el.
|
inline |
Get the value of the DE modulus.
Definition at line 370 of file config_structure.inl.
|
inline |
Flag for whether to solve the energy equation for incompressible flows.
Definition at line 862 of file config_structure.inl.
|
inline |
Get the value of the frestream temperature.
Definition at line 486 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream energy.
Definition at line 548 of file config_structure.inl.
|
inline |
Get the value of the reference pressure for non-dimensionalization.
Definition at line 520 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
Definition at line 276 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
Definition at line 268 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
Definition at line 274 of file config_structure.inl.
|
inline |
Only halg of the engine is in the compputational grid.
TRUE if the engine is complete; otherwise FALSE. Definition at line 1521 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
Definition at line 266 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
Definition at line 272 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
Definition at line 270 of file config_structure.inl.
| su2double CConfig::GetEngineInflow_Target | ( | string | val_marker | ) |
Get the target (pressure, massflow, etc) at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
Definition at line 8086 of file config_structure.cpp.
| su2double CConfig::GetEnthalpy_Formation | ( | unsigned short | iSpecies | ) |
Provides the formation enthalpy of the specified species at standard conditions.
| su2double* CConfig::GetEnthalpy_Formation | ( | void | ) |
Provides the formation enthalpy of the specified species at standard conditions.
|
inline |
Get the entropy fix.
Definition at line 1028 of file config_structure.inl.
|
inline |
Information about computing and plotting the equivalent area distribution.
TRUE or FALSE depending if we are computing the equivalent area. Definition at line 1294 of file config_structure.inl.
|
inline |
Get boolean for using Persson's shock capturing method in Euler flow DG-FEM.
Definition at line 1867 of file config_structure.inl.
|
inline |
Get information about whether to use fixed CL mode.
TRUE if fixed CL mode is active; otherwise FALSE. Definition at line 1753 of file config_structure.inl.
| su2double CConfig::GetExhaust_Force | ( | string | val_marker | ) |
Get the force balance at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8205 of file config_structure.cpp.
| su2double CConfig::GetExhaust_GrossThrust | ( | string | val_marker | ) |
Get the gross thrust at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8198 of file config_structure.cpp.
| su2double CConfig::GetExhaust_MassFlow | ( | string | val_marker | ) |
Get the massflow at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8177 of file config_structure.cpp.
| su2double CConfig::GetExhaust_Power | ( | string | val_marker | ) |
Get the power at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8212 of file config_structure.cpp.
| su2double CConfig::GetExhaust_Pressure | ( | string | val_marker | ) |
Get the back pressure (static) at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8163 of file config_structure.cpp.
| su2double CConfig::GetExhaust_Pressure_Target | ( | string | val_index | ) |
Get the total pressure at an nacelle boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7628 of file config_structure.cpp.
| su2double CConfig::GetExhaust_Temperature | ( | string | val_marker | ) |
Get the temperature (static) at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8170 of file config_structure.cpp.
| su2double CConfig::GetExhaust_Temperature_Target | ( | string | val_index | ) |
Get the total temperature at a nacelle boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7621 of file config_structure.cpp.
| su2double CConfig::GetExhaust_TotalPressure | ( | string | val_marker | ) |
Get the total pressure at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8184 of file config_structure.cpp.
| su2double CConfig::GetExhaust_TotalTemperature | ( | string | val_marker | ) |
Get the total temperature at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8191 of file config_structure.cpp.
|
inline |
Get the current external iteration number.
Definition at line 308 of file config_structure.inl.
|
inline |
Get the current internal iteration number.
Definition at line 310 of file config_structure.inl.
|
inline |
Heat solver zone with extra screen output.
Definition at line 354 of file config_structure.inl.
|
inline |
Creates a tecplot file to visualize the partition made by the DDC software.
TRUE if the partition is going to be plotted; otherwise FALSE. Definition at line 352 of file config_structure.inl.
|
inline |
Get extra relaxation factor coefficients for the Giels BC.
Definition at line 1206 of file config_structure.inl.
|
inline |
Get the value of the reference viscosity for non-dimensionalization.
Definition at line 530 of file config_structure.inl.
|
inline |
Get the name of the file with the element properties for structural problems.
Definition at line 414 of file config_structure.inl.
|
inline |
Get the value of the vector that connects the cartesian axis with a sherical or cylindrical one.
Definition at line 440 of file config_structure.inl.
|
inline |
Get the kind of FFD Blending function.
Definition at line 1939 of file config_structure.inl.
|
inline |
Get the kind BSpline Order in i,j,k direction.
Definition at line 1941 of file config_structure.inl.
|
inline |
Get the required continuity level at the surface intersection with the FFD.
Definition at line 781 of file config_structure.inl.
|
inline |
Get the coordinate system that we are going to use to define the FFD.
Definition at line 783 of file config_structure.inl.
|
inline |
plane of the FFD (I axis) that should be fixed.
| [in] | val_index | - Index of the arrray with all the planes in the I direction that should be fixed. |
Definition at line 813 of file config_structure.inl.
|
inline |
plane of the FFD (J axis) that should be fixed.
| [in] | val_index | - Index of the arrray with all the planes in the J direction that should be fixed. |
Definition at line 815 of file config_structure.inl.
|
inline |
plane of the FFD (K axis) that should be fixed.
| [in] | val_index | - Index of the arrray with all the planes in the K direction that should be fixed. |
Definition at line 817 of file config_structure.inl.
|
inline |
Define the FFD box with a symetry plane.
TRUE if there is a symmetry plane in the FFD; otherwise FALSE. Definition at line 1056 of file config_structure.inl.
|
inline |
Get the tolerance of the point inversion algorithm.
Definition at line 1737 of file config_structure.inl.
|
inline |
Get the FFD Tag of a particular design variable.
| [in] | val_dv | - Number of the design variable that we want to read. |
Definition at line 771 of file config_structure.inl.
|
inline |
Get final Outlet Pressure value for the ramp.
Definition at line 1196 of file config_structure.inl.
|
inline |
Get the angular velocity of the mesh about the z-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 936 of file config_structure.inl.
|
inline |
Get the index of the finest grid.
Definition at line 731 of file config_structure.inl.
|
inline |
Value of the azimuthal line to fix due to a misalignments of the nearfield.
Definition at line 1573 of file config_structure.inl.
|
inline |
Get information about whether to use fixed CL mode.
TRUE if fixed CL mode is active; otherwise FALSE. Definition at line 1749 of file config_structure.inl.
|
inline |
Get information about whether to use fixed CL mode.
TRUE if fixed CL mode is active; otherwise FALSE. Definition at line 1751 of file config_structure.inl.
|
inline |
Get the name of the file with the flow variables.
Definition at line 1453 of file config_structure.inl.
| su2double CConfig::GetFlowAngleIn_BC | ( | ) |
Get the inlet flow angle imposed as BC for internal flow.
Definition at line 7872 of file config_structure.cpp.
| su2double CConfig::GetFlowLoad_Value | ( | string | val_index | ) |
Get the force value at an load boundary.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8415 of file config_structure.cpp.
|
inline |
Get the value of the reference force for non-dimensionalization.
Definition at line 534 of file config_structure.inl.
|
inline |
Set freestream turbonormal for initializing solution.
Definition at line 1180 of file config_structure.inl.
|
inline |
Get the Froude number for free surface problems.
Definition at line 613 of file config_structure.inl.
|
inline |
Provides information about the way in which the limiter will be treated by the disc. adjoint method.
FALSE means that the limiter computation is included. Definition at line 1611 of file config_structure.inl.
|
inline |
Provides information about the way in which the turbulence will be treated by the cont. adjoint method.
FALSE means that the adjoint turbulence equations will be used. Definition at line 1607 of file config_structure.inl.
|
inline |
Provides information about the way in which the turbulence will be treated by the disc. adjoint method.
FALSE means that the adjoint turbulence equations will be used. Definition at line 1609 of file config_structure.inl.
|
inline |
Check if the simulation we are running is a FSI simulation.
Definition at line 1871 of file config_structure.inl.
|
inline |
Get the current FSI iteration number.
Definition at line 312 of file config_structure.inl.
|
inline |
Get the value of the Gamma of fluid (ratio of specific heats).
Definition at line 436 of file config_structure.inl.
|
inline |
Get the value of specific gas constant.
Definition at line 446 of file config_structure.inl.
|
inline |
Get the reference value for the specific gas constant.
Definition at line 482 of file config_structure.inl.
|
inline |
Get the value of specific gas constant.
Definition at line 448 of file config_structure.inl.
|
inline |
Get Description of the geometry to be analyzed.
Definition at line 348 of file config_structure.inl.
|
inline |
Get the location of the waterline.
Definition at line 1268 of file config_structure.inl.
|
inline |
Geometric conditions for the structural solver.
Definition at line 406 of file config_structure.inl.
|
inline |
Get the king of evaluation in the geometrical module.
Definition at line 753 of file config_structure.inl.
| su2double * CConfig::GetGiles_FlowDir | ( | string | val_marker | ) |
Get the Flowdir for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 7769 of file config_structure.cpp.
| su2double CConfig::GetGiles_RelaxFactorAverage | ( | string | val_marker | ) |
Get the relax factor for the average component for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 7755 of file config_structure.cpp.
| su2double CConfig::GetGiles_RelaxFactorFourier | ( | string | val_marker | ) |
Get the relax factor for the fourier component for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 7762 of file config_structure.cpp.
| su2double CConfig::GetGiles_Var1 | ( | string | val_marker | ) |
Get the var 1 for the Giels BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 7734 of file config_structure.cpp.
| su2double CConfig::GetGiles_Var2 | ( | string | val_marker | ) |
Get the var 2 for the Giles boundary.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 7748 of file config_structure.cpp.
|
inline |
Get information about the gravity force.
TRUE if it uses the gravity force; otherwise FALSE. Definition at line 1591 of file config_structure.inl.
|
inline |
Get information about the grid movement.
TRUE if there is a grid movement; otherwise FALSE. Definition at line 1577 of file config_structure.inl.
|
inline |
Get the number of linear smoothing iterations for mesh deformation.
Definition at line 1034 of file config_structure.inl.
|
inline |
Get the number of nonlinear increments for mesh deformation.
Definition at line 1036 of file config_structure.inl.
|
inline |
Value of the gust amplitude.
Definition at line 1729 of file config_structure.inl.
|
inline |
Value of the location ath which the gust begins.
Definition at line 1733 of file config_structure.inl.
|
inline |
Value of the time at which to begin the gust.
Definition at line 1731 of file config_structure.inl.
|
inline |
Get the gust direction.
Definition at line 1723 of file config_structure.inl.
|
inline |
Value of the number of gust periods.
Definition at line 1727 of file config_structure.inl.
|
inline |
Get the type of gust to simulate.
Definition at line 1721 of file config_structure.inl.
|
inline |
Value of the gust wavelength.
Definition at line 1725 of file config_structure.inl.
|
inline |
Retrieves the period of oscillations to be used with Harmonic Balance.
Definition at line 298 of file config_structure.inl.
|
inline |
Get if harmonic balance source term is to be preconditioned.
Definition at line 46 of file config_structure.inl.
|
inline |
Get the name of the file with the wave variables.
Definition at line 1465 of file config_structure.inl.
|
inline |
Get the reference value for the heat flux.
Definition at line 478 of file config_structure.inl.
|
inline |
Get the value of the reference viscosity for non-dimensionalization.
Definition at line 528 of file config_structure.inl.
|
inline |
Retrieve the ofstream of the history file for the current zone.
Definition at line 1963 of file config_structure.inl.
|
inline |
Provides information about the the nodes that are going to be moved on a deformation volumetric grid deformation.
TRUE means that only the points on the FFD box will be moved. Definition at line 1619 of file config_structure.inl.
|
inline |
Get the the coordinates where of the box where the grid is going to be deformed.
Definition at line 338 of file config_structure.inl.
|
inline |
Get the values of the CFL adapation.
Definition at line 40 of file config_structure.inl.
|
inline |
Get the current instance.
Definition at line 1821 of file config_structure.inl.
|
inline |
Get the value of the initial density for incompressible flows.
Definition at line 472 of file config_structure.inl.
|
inline |
Get the value of the reference density for custom incompressible non-dimensionalization.
Definition at line 466 of file config_structure.inl.
|
inline |
Flag for whether the local boundary normal is used as the flow direction for an incompressible pressure inlet.
FALSE means the prescribed flow direction is used. Definition at line 1174 of file config_structure.inl.
|
inline |
Get the value of the initial temperature for incompressible flows.
Definition at line 476 of file config_structure.inl.
|
inline |
Get the value of the reference temperature for custom incompressible non-dimensionalization.
Definition at line 470 of file config_structure.inl.
|
inline |
Get the value of the initial velocity for incompressible flows.
Definition at line 474 of file config_structure.inl.
|
inline |
Get the value of the reference velocity for custom incompressible non-dimensionalization.
Definition at line 468 of file config_structure.inl.
| su2double CConfig::GetIncInlet_BC | ( | ) |
Get the inlet velocity or pressure imposed for incompressible flow.
Definition at line 7893 of file config_structure.cpp.
|
inline |
Get the value of the criteria for applying incremental loading.
Definition at line 1865 of file config_structure.inl.
|
inline |
Provides information about using an inconsistent (primal/dual) discrete adjoint formulation.
FALSE means that the adjoint use the same numerical methods than the primal problem. Definition at line 1613 of file config_structure.inl.
| su2double CConfig::GetIncPressureOut_BC | ( | ) |
Get the outlet pressure imposed as BC for incompressible flow.
Definition at line 7937 of file config_structure.cpp.
|
inline |
Check if we want to apply an incremental load to the nonlinear structural simulation.
TRUE means that the load is to be applied in increments. Definition at line 1861 of file config_structure.inl.
| su2double CConfig::GetIncTemperature_BC | ( | ) |
Get the inlet temperature imposed as BC for incompressible flow.
Definition at line 7918 of file config_structure.cpp.
| su2double CConfig::GetInflow_Force | ( | string | val_marker | ) |
Get the force balance at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8142 of file config_structure.cpp.
| su2double CConfig::GetInflow_Mach | ( | string | val_marker | ) |
Get the fan face Mach number at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8156 of file config_structure.cpp.
| su2double CConfig::GetInflow_MassFlow | ( | string | val_marker | ) |
Get the mass flow rate at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8100 of file config_structure.cpp.
| su2double CConfig::GetInflow_Power | ( | string | val_marker | ) |
Get the power at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8149 of file config_structure.cpp.
| su2double CConfig::GetInflow_Pressure | ( | string | val_marker | ) |
Get the back pressure (static) at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8093 of file config_structure.cpp.
| su2double CConfig::GetInflow_RamDrag | ( | string | val_marker | ) |
Get the ram drag at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8135 of file config_structure.cpp.
| su2double CConfig::GetInflow_ReverseMassFlow | ( | string | val_marker | ) |
Get the percentage of reverse flow at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8107 of file config_structure.cpp.
|
inline |
Get the percentage of reverse flow at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
Definition at line 68 of file config_structure.inl.
| su2double CConfig::GetInflow_Temperature | ( | string | val_marker | ) |
Get the temperature (static) at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8121 of file config_structure.cpp.
| su2double CConfig::GetInflow_TotalPressure | ( | string | val_marker | ) |
Get the total pressure at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8114 of file config_structure.cpp.
| su2double CConfig::GetInflow_TotalTemperature | ( | string | val_marker | ) |
Get the total temperature at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 8128 of file config_structure.cpp.
|
inline |
Get the value of the non-dimensionalized actuator disk turbulence intensity.
Definition at line 566 of file config_structure.inl.
| su2double CConfig::GetInitial_Gas_Composition | ( | unsigned short | iSpecies | ) |
Provides the molar mass of each species present in multi species fluid.
|
inline |
Get name of the input file for the specified inlet profile.
Definition at line 1168 of file config_structure.inl.
| su2double * CConfig::GetInlet_FlowDir | ( | string | val_index | ) |
Get the flow direction unit vector at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7663 of file config_structure.cpp.
| su2double CConfig::GetInlet_Pressure | ( | string | val_index | ) |
Get the pressure at a supersonic inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7677 of file config_structure.cpp.
|
inline |
Check if the inlet profile(s) are specified in an input file.
Definition at line 1166 of file config_structure.inl.
|
inline |
Get the tolerance used for matching two points on a specified inlet.
Definition at line 1170 of file config_structure.inl.
| su2double CConfig::GetInlet_Ptotal | ( | string | val_index | ) |
Get the total pressure at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7649 of file config_structure.cpp.
| su2double CConfig::GetInlet_Temperature | ( | string | val_index | ) |
Get the temperature at a supersonic inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7670 of file config_structure.cpp.
| su2double CConfig::GetInlet_Ttotal | ( | string | val_index | ) |
Get the total temperature at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7642 of file config_structure.cpp.
| su2double * CConfig::GetInlet_Velocity | ( | string | val_index | ) |
Get the velocity vector at a supersonic inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7684 of file config_structure.cpp.
|
inline |
Check if values passed to the BC_HeatFlux-Routine are already integrated.
Definition at line 1933 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream intermittency.
Definition at line 570 of file config_structure.inl.
|
inline |
Get the current internal iteration number.
Definition at line 314 of file config_structure.inl.
|
inline |
Information about computing and plotting the equivalent area distribution.
TRUE or FALSE depending if we are computing the equivalent area. Definition at line 1296 of file config_structure.inl.
|
inline |
Information about computing and plotting the equivalent area distribution.
TRUE or FALSE depending if we are computing the equivalent area. Definition at line 1298 of file config_structure.inl.
| bool CConfig::GetIonization | ( | void | ) |
Indicates whether electron gas is present in the gas mixture.
| su2double CConfig::GetIsothermal_Temperature | ( | string | val_index | ) |
Get the wall temperature (static) at an isothermal boundary.
| [in] | val_index | - Index corresponding to the isothermal boundary. |
Definition at line 7960 of file config_structure.cpp.
| bool CConfig::GetIsothermalWall | ( | void | ) |
Get information about the isothermal wall condition.
TRUE if it is a isothermal wall condition; otherwise FALSE.
|
inline |
Number of iterations to average (reverse time integration).
Definition at line 326 of file config_structure.inl.
|
inline |
Number of iterations to evaluate dCL_dAlpha.
Definition at line 1769 of file config_structure.inl.
|
inline |
Get the value of iterations to re-evaluate the angle of attack.
Definition at line 1765 of file config_structure.inl.
|
inline |
Get the value of iterations to re-evaluate the angle of attack.
Definition at line 1763 of file config_structure.inl.
|
inline |
Provides the number of varaibles.
Definition at line 280 of file config_structure.inl.
|
inline |
Function to make available whether or not only the exact Jacobian of the spatial discretization must be computed.
Definition at line 1929 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the low order method (center scheme).
Definition at line 1140 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the Lax method (center scheme).
Definition at line 1122 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the high order method (center scheme).
Definition at line 1142 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the JST method (center scheme).
Definition at line 1124 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the JST method (center scheme).
Definition at line 1128 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the high order method (center scheme).
Definition at line 1144 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the JST method (center scheme).
Definition at line 1126 of file config_structure.inl.
|
inline |
Value of the calibrated constant for the JST-like method (center scheme).
Definition at line 1130 of file config_structure.inl.
|
inline |
Get the kind of inlet boundary condition treatment (total conditions or mass flow).
Definition at line 1178 of file config_structure.inl.
|
inline |
Get the kind of adaptation technique.
Definition at line 1058 of file config_structure.inl.
|
inline |
Get the kind of scheme (aliased or non-aliased) to be used in the predictor step of ADER-DG.
Definition at line 1084 of file config_structure.inl.
|
inline |
Get the kind of preconditioner for the implicit solver.
Definition at line 1016 of file config_structure.inl.
|
inline |
Get the kind of solver for the implicit solver.
Definition at line 1014 of file config_structure.inl.
|
inline |
Get the kind of marker analyze marker (area-averaged, mass flux averaged, etc).
Definition at line 1793 of file config_structure.inl.
|
inline |
Get the kind of mixing process for averaging quantities at the boundaries.
Definition at line 1182 of file config_structure.inl.
|
inline |
Get kind of center scheme for the convective terms.
Definition at line 1066 of file config_structure.inl.
|
inline |
Get the kind of center convective numerical scheme for the adjoint flow equations.
Definition at line 1136 of file config_structure.inl.
|
inline |
Get the kind of center convective numerical scheme for the adjoint turbulence equations.
Definition at line 1158 of file config_structure.inl.
|
inline |
Get the kind of center convective numerical scheme for the flow equations.
Definition at line 1102 of file config_structure.inl.
| unsigned short CConfig::GetKind_Centered_Template | ( | void | ) |
Get the kind of center convective numerical scheme for the plasma equations.
|
inline |
Get the kind of center convective numerical scheme for the turbulence equations.
Definition at line 1150 of file config_structure.inl.
|
inline |
Get the value of the thermal conductivity model.
Definition at line 874 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme.
Definition at line 1064 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme for the adjoint flow equations (centered or upwind).
Definition at line 1134 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme for the adjoint turbulence equations (centered or upwind).
Definition at line 1156 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme for the flow equations (finite element).
Definition at line 1098 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme for the flow equations (centered or upwind).
Definition at line 1096 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme for the heat equation.
Definition at line 1162 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme for the template equations (centered or upwind).
Definition at line 1100 of file config_structure.inl.
|
inline |
Get the kind of convective numerical scheme for the turbulence equations (upwind).
Definition at line 1148 of file config_structure.inl.
| unsigned short CConfig::GetKind_Data_Giles | ( | string | val_marker | ) |
Get Kind Data for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 7776 of file config_structure.cpp.
| unsigned short CConfig::GetKind_Data_Riemann | ( | string | val_marker | ) |
Get Kind Data of Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 7726 of file config_structure.cpp.
|
inline |
Get the kind of solver for the implicit solver.
Definition at line 982 of file config_structure.inl.
|
inline |
Get the kind of preconditioner for the implicit solver.
Definition at line 1022 of file config_structure.inl.
|
inline |
Option to define the density model for incompressible flows.
Definition at line 860 of file config_structure.inl.
|
inline |
Get the kind of preconditioner for the implicit solver.
Definition at line 1020 of file config_structure.inl.
|
inline |
Get the kind of solver for the implicit solver.
Definition at line 1018 of file config_structure.inl.
|
inline |
Get the kind of inlet boundary condition treatment (total conditions or mass flow).
Definition at line 1176 of file config_structure.inl.
|
inline |
Get the kind of shock capturing method in FEM DG solver.
Definition at line 1118 of file config_structure.inl.
|
inline |
Get the kind of finite element convective numerical scheme for the flow equations.
Definition at line 1116 of file config_structure.inl.
|
inline |
Fluid model that we are using.
Definition at line 856 of file config_structure.inl.
|
inline |
free stream option to initialize the solution
Definition at line 858 of file config_structure.inl.
|
inline |
Gas model that we are using.
Definition at line 854 of file config_structure.inl.
|
inline |
Get the kind of method for computation of spatial gradients.
Definition at line 978 of file config_structure.inl.
|
inline |
Get the type of dynamic mesh motion.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 906 of file config_structure.inl.
|
inline |
Get the Kind of Hybrid RANS/LES.
Definition at line 1953 of file config_structure.inl.
| unsigned short CConfig::GetKind_Inc_Inlet | ( | string | val_marker | ) |
Get the type of incompressible inlet from the list.
Definition at line 7635 of file config_structure.cpp.
|
inline |
free stream option to initialize the solution
Definition at line 864 of file config_structure.inl.
|
inline |
Get the kind of inlet boundary condition treatment (total conditions or mass flow).
Definition at line 1164 of file config_structure.inl.
|
inline |
Get the kind of solver for the implicit solver.
Definition at line 980 of file config_structure.inl.
|
inline |
Get the kind of preconditioner for the implicit solver.
Definition at line 986 of file config_structure.inl.
|
inline |
Get the kind of matrix coloring used for the sparse Jacobian computation.
Definition at line 1120 of file config_structure.inl.
|
inline |
Get the kind of mixing process for averaging quantities at the boundaries.
Definition at line 1210 of file config_structure.inl.
|
inline |
Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.
Definition at line 1274 of file config_structure.inl.
|
inline |
Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.
Definition at line 1272 of file config_structure.inl.
|
inline |
Get the kind of mixing process for averaging quantities at the boundaries.
Definition at line 1184 of file config_structure.inl.
|
inline |
Governing equations of the flow (it can be different from the run time equation).
| [in] | val_zone | - Zone where the soler is applied. |
Definition at line 850 of file config_structure.inl.
|
inline |
Get the Kind of Roe Low Dissipation Scheme for Unsteady flows.
Definition at line 1955 of file config_structure.inl.
|
inline |
Get the kind of sensitivity smoothing technique.
Definition at line 1282 of file config_structure.inl.
|
inline |
Get the kind of the subgrid scale model.
Definition at line 1605 of file config_structure.inl.
|
inline |
Get the method for limiting the spatial gradients.
Definition at line 1104 of file config_structure.inl.
|
inline |
Get the method for limiting the spatial gradients.
Definition at line 1112 of file config_structure.inl.
|
inline |
Get the method for limiting the spatial gradients.
Definition at line 1110 of file config_structure.inl.
|
inline |
Get the method for limiting the spatial gradients.
Definition at line 1106 of file config_structure.inl.
|
inline |
Get the method for limiting the spatial gradients.
Definition at line 1108 of file config_structure.inl.
|
inline |
Governing equations of the flow (it can be different from the run time equation).
| [in] | val_zone | - Zone where the soler is applied. |
Definition at line 846 of file config_structure.inl.
|
inline |
Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 1092 of file config_structure.inl.
|
inline |
Get the kind of turbomachinery architecture.
Definition at line 1214 of file config_structure.inl.
|
inline |
Get the kind of SU2 software component.
Definition at line 282 of file config_structure.inl.
|
inline |
Get the kind of time integration method.
Definition at line 1062 of file config_structure.inl.
|
inline |
Get the kind of integration scheme (explicit or implicit) for the adjoint flow equations.
Definition at line 1132 of file config_structure.inl.
|
inline |
Get the kind of integration scheme (explicit or implicit) for the adjoint turbulence equations.
Definition at line 1154 of file config_structure.inl.
|
inline |
Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 1090 of file config_structure.inl.
|
inline |
Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 1082 of file config_structure.inl.
|
inline |
Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 1086 of file config_structure.inl.
| unsigned short CConfig::GetKind_TimeIntScheme_Template | ( | void | ) |
Get the kind of integration scheme (explicit or implicit) for the template equations.
|
inline |
Get the kind of integration scheme (implicit) for the turbulence equations.
Definition at line 1146 of file config_structure.inl.
|
inline |
Get the kind of time stepping for the heat equation.
Definition at line 1088 of file config_structure.inl.
|
inline |
Get the kind of the transition model.
Definition at line 1603 of file config_structure.inl.
|
inline |
Get the kind of transfer method we want to use for multiphysics problems.
Definition at line 1094 of file config_structure.inl.
|
inline |
Get the kind of the turbulence model.
Definition at line 1601 of file config_structure.inl.
|
inline |
Get the kind of turbomachinery architecture.
Definition at line 1212 of file config_structure.inl.
| unsigned short CConfig::GetKind_TurboPerf | ( | unsigned short | index | ) |
get marker kind for Turbomachinery performance calculation.
|
inline |
Get kind of upwind scheme for the convective terms.
Definition at line 1068 of file config_structure.inl.
|
inline |
Get the kind of upwind convective numerical scheme for the adjoint flow equations.
Definition at line 1138 of file config_structure.inl.
|
inline |
Get the kind of upwind convective numerical scheme for the adjoint turbulence equations.
Definition at line 1160 of file config_structure.inl.
|
inline |
Get the kind of upwind convective numerical scheme for the flow equations.
Definition at line 1114 of file config_structure.inl.
|
inline |
Get the kind of upwind convective numerical scheme for the turbulence equations.
Definition at line 1152 of file config_structure.inl.
|
inline |
Get the value of the viscosity model.
Definition at line 872 of file config_structure.inl.
|
inline |
Get the interpolation method used for matching between zones.
Definition at line 1875 of file config_structure.inl.
|
inline |
Get the basis function to use for radial basis function interpolation for FSI.
Definition at line 1877 of file config_structure.inl.
|
inline |
Get the value of the B constant in the Knowles material model.
Definition at line 372 of file config_structure.inl.
|
inline |
Get the value of the N constant in the Knowles material model.
Definition at line 374 of file config_structure.inl.
|
inline |
Get the value of the thermal conductivity.
Definition at line 880 of file config_structure.inl.
|
inline |
Get the value of the non-dimensional thermal conductivity.
Definition at line 882 of file config_structure.inl.
|
inline |
Get the value of the reference length for non-dimensionalization. This value should always be 1 internally, and is not user-specified.
Definition at line 510 of file config_structure.inl.
|
inline |
Get the value of the Reynolds length.
Definition at line 578 of file config_structure.inl.
|
inline |
Freeze the value of the limiter after a number of iterations.
Definition at line 607 of file config_structure.inl.
|
inline |
Get min error of the linear solver for the implicit formulation.
Definition at line 990 of file config_structure.inl.
|
inline |
Get the ILU fill-in level for the linear solver.
Definition at line 998 of file config_structure.inl.
|
inline |
Get max number of iterations of the linear solver for the implicit formulation.
Definition at line 994 of file config_structure.inl.
|
inline |
Get restart frequency of the linear solver for the implicit formulation.
Definition at line 1000 of file config_structure.inl.
| su2double * CConfig::GetLoad_Dir | ( | string | val_index | ) |
Get the force direction at a loaded boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8380 of file config_structure.cpp.
| su2double CConfig::GetLoad_Dir_Multiplier | ( | string | val_index | ) |
Get the force multiplier at a load boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8359 of file config_structure.cpp.
| su2double CConfig::GetLoad_Dir_Value | ( | string | val_index | ) |
Get the force value at a load boundary defined in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8352 of file config_structure.cpp.
|
inline |
Get the sine load properties.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 1853 of file config_structure.inl.
| su2double CConfig::GetLoad_Sine_Amplitude | ( | string | val_index | ) |
Get the amplitude of the sine-wave at a load boundary defined in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8394 of file config_structure.cpp.
| su2double * CConfig::GetLoad_Sine_Dir | ( | string | val_index | ) |
Get the force direction at a sine-wave loaded boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8408 of file config_structure.cpp.
| su2double CConfig::GetLoad_Sine_Frequency | ( | string | val_index | ) |
Get the frequency of the sine-wave at a load boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8401 of file config_structure.cpp.
| su2double CConfig::GetLoad_Value | ( | string | val_index | ) |
Get the force value at an load boundary.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 8338 of file config_structure.cpp.
|
inline |
Get the airfoil sections in the slicing process.
| [in] | val_section | - Index of the section. |
Definition at line 803 of file config_structure.inl.
|
inline |
Get information about writing a volume solution file.
TRUE means that a volume solution file will be written. Definition at line 1647 of file config_structure.inl.
|
inline |
Get the value of the Mach number (velocity divided by speed of sound).
Definition at line 434 of file config_structure.inl.
|
inline |
Get the mach number based on the mesh velocity and freestream quantities.
Definition at line 910 of file config_structure.inl.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1304 of file config_structure.inl.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1306 of file config_structure.inl.
|
inline |
Get the plotting information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 1375 of file config_structure.inl.
|
inline |
Get the design information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 1367 of file config_structure.inl.
|
inline |
Get the DV information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be affected by design variables. |
Definition at line 1387 of file config_structure.inl.
|
inline |
Get the monitoring information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 1365 of file config_structure.inl.
|
inline |
Get the kind of boundary for each marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
Definition at line 1329 of file config_structure.inl.
|
inline |
Get the MixingPlane interface information for a marker val_marker.
| [in] | val_marker | value of the marker on the grid. |
Definition at line 1385 of file config_structure.inl.
|
inline |
Get the monitoring information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 1363 of file config_structure.inl.
|
inline |
Get the motion information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 1389 of file config_structure.inl.
|
inline |
Get an internal index that identify the periodic boundary conditions.
| [in] | val_marker | - Value of the marker that correspond with the periodic boundary. |
Definition at line 1361 of file config_structure.inl.
|
inline |
Get the plotting information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 1373 of file config_structure.inl.
|
inline |
Get the Python customization for a marker val_marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
Definition at line 1391 of file config_structure.inl.
|
inline |
Get the send-receive information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 1369 of file config_structure.inl.
|
inline |
Get the tag if the iMarker defined in the geometry file.
| [in] | val_tag | - Value of the tag in which we are interested. |
Definition at line 1322 of file config_structure.inl.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1302 of file config_structure.inl.
|
inline |
Get the Turbomachinery information for a marker val_marker.
| [in] | val_marker | value of the marker on the grid. |
Definition at line 1381 of file config_structure.inl.
|
inline |
Get the Turbomachinery flag information for a marker val_marker.
| [in] | val_marker | value of the marker on the grid. |
Definition at line 1383 of file config_structure.inl.
|
inline |
Get the FSI interface information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 1377 of file config_structure.inl.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1320 of file config_structure.inl.
| unsigned short CConfig::GetMarker_CfgFile_ActDiskOutlet | ( | string | val_marker | ) |
Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet).
Definition at line 7543 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Analyze | ( | string | val_marker | ) |
Get the plotting information from the config definition for the marker val_marker.
Definition at line 6511 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Designing | ( | string | val_marker | ) |
Get the monitoring information from the config definition for the marker val_marker.
Definition at line 6497 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_DV | ( | string | val_marker | ) |
Get the DV information from the config definition for the marker val_marker.
Definition at line 6547 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_EngineExhaust | ( | string | val_marker | ) |
Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet).
Definition at line 7559 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_GeoEval | ( | string | val_marker | ) |
Get the monitoring information from the config definition for the marker val_marker.
Definition at line 6490 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_KindBC | ( | string | val_marker | ) |
Get the boundary information (kind of boundary) in the config information of the marker val_marker.
Definition at line 6476 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_MixingPlaneInterface | ( | string | val_marker | ) |
Get the MixingPlane interface information from the config definition for the marker val_marker.
Definition at line 6540 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Monitoring | ( | string | val_marker | ) |
Get the monitoring information from the config definition for the marker val_marker.
Definition at line 6483 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Moving | ( | string | val_marker | ) |
Get the motion information from the config definition for the marker val_marker.
Definition at line 6554 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_PerBound | ( | string | val_marker | ) |
Get the periodic information from the config definition of the marker val_marker.
Definition at line 6568 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Plotting | ( | string | val_marker | ) |
Get the plotting information from the config definition for the marker val_marker.
Definition at line 6504 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_PyCustom | ( | string | val_marker | ) |
Get the Python customization information from the config definition for the marker val_marker.
Definition at line 6561 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_TagBound | ( | string | val_marker | ) |
Get the index in the config information of the marker val_marker.
Definition at line 6460 of file config_structure.cpp.
| string CConfig::GetMarker_CfgFile_TagBound | ( | unsigned short | val_marker | ) |
Get the name in the config information of the marker number val_marker.
Definition at line 6472 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Turbomachinery | ( | string | val_marker | ) |
Get the TurboPerformance information from the config definition for the marker val_marker.
Definition at line 6526 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_TurbomachineryFlag | ( | string | val_marker | ) |
Get the TurboPerformance flag information from the config definition for the marker val_marker.
Definition at line 6533 of file config_structure.cpp.
| unsigned short CConfig::GetMarker_CfgFile_ZoneInterface | ( | string | val_marker | ) |
Get the FSI interface information from the config definition for the marker val_marker.
Definition at line 6519 of file config_structure.cpp.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1310 of file config_structure.inl.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1308 of file config_structure.inl.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1314 of file config_structure.inl.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1312 of file config_structure.inl.
| unsigned short CConfig::GetMarker_Moving | ( | string | val_marker | ) |
Get the internal index for a moving boundary val_marker.
Definition at line 7593 of file config_structure.cpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1316 of file config_structure.inl.
|
inline |
Get the number of FSI interface markers val_marker.
| [in] | void. |
Definition at line 1379 of file config_structure.inl.
|
inline |
get outlet bounds name for Turbomachinery performance calculation.
Definition at line 1262 of file config_structure.inl.
| unsigned short CConfig::GetMarker_Periodic_Donor | ( | string | val_marker | ) |
Get the rotationally periodic donor marker for boundary val_marker.
Definition at line 7413 of file config_structure.cpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 1318 of file config_structure.inl.
|
inline |
Get the marker shroud.
Definition at line 1240 of file config_structure.inl.
|
inline |
get inlet bounds name for Turbomachinery performance calculation.
Definition at line 1258 of file config_structure.inl.
|
inline |
get outlet bounds name for Turbomachinery performance calculation.
Definition at line 1260 of file config_structure.inl.
| int CConfig::GetMarker_ZoneInterface | ( | string | val_marker | ) |
Get the name of the marker val_marker.
Definition at line 6575 of file config_structure.cpp.
|
inline |
Get the vector of free stream mass fraction values.
Definition at line 576 of file config_structure.inl.
|
inline |
Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures).
TRUE if the mesh is matching, FALSE otherwise. Definition at line 1809 of file config_structure.inl.
|
inline |
Compressibility/incompressibility of the solids analysed using the structural solver.
Definition at line 402 of file config_structure.inl.
|
inline |
Get the Material Density.
Definition at line 394 of file config_structure.inl.
|
inline |
Compressibility/incompressibility of the solids analysed using the structural solver.
Definition at line 404 of file config_structure.inl.
|
inline |
Get the Courant Friedrich Levi number for unsteady simulations.
Definition at line 763 of file config_structure.inl.
|
inline |
Get the maximum velocity^2 in the domain for the incompressible preconditioner.
Definition at line 1945 of file config_structure.inl.
|
inline |
Get the minimum value of Beta for Roe-Turkel preconditioner.
Definition at line 976 of file config_structure.inl.
|
inline |
Get the format of the input/output grid.
Definition at line 1433 of file config_structure.inl.
|
inline |
Get name of the input grid.
Definition at line 1429 of file config_structure.inl.
|
inline |
Get name of the output grid, this parameter is important for grid adaptation and deformation.
Definition at line 1431 of file config_structure.inl.
|
inline |
Get the number of implicit Jacobi smoothings of the correction in a multigrid strategy.
| [in] | val_mesh | - Index of the grid. |
Definition at line 829 of file config_structure.inl.
|
inline |
Get the number of post-smoothings in a multigrid strategy.
| [in] | val_mesh | - Index of the grid. |
Definition at line 824 of file config_structure.inl.
|
inline |
Get the number of pre-smoothings in a multigrid strategy.
| [in] | val_mesh | - Index of the grid. |
Definition at line 819 of file config_structure.inl.
|
inline |
Get the kind of multigrid (V or W).
Definition at line 751 of file config_structure.inl.
|
inline |
Value of the minimum residual value (log10 scale).
Definition at line 1531 of file config_structure.inl.
|
inline |
Value of the minimum flow residual value for BGS applications (log10 scale).
Definition at line 1893 of file config_structure.inl.
|
inline |
Value of the minimum flow residual value for BGS applications (log10 scale).
Definition at line 1897 of file config_structure.inl.
|
inline |
Value of the minimum residual value for FSI applications (log10 scale).
Definition at line 1889 of file config_structure.inl.
|
inline |
Get the minimum value of Beta for Roe-Turkel preconditioner.
Definition at line 974 of file config_structure.inl.
|
inline |
Get mixedout coefficients.
Definition at line 1204 of file config_structure.inl.
|
inline |
Get the value of the frestream temperature.
Definition at line 494 of file config_structure.inl.
|
inline |
Get the value of the frestream temperature.
Definition at line 496 of file config_structure.inl.
| su2double CConfig::GetMolar_Mass | ( | unsigned short | iSpecies | ) |
Provides the molar mass of each species present in multi species fluid.
| su2double* CConfig::GetMolar_Mass | ( | void | ) |
Provides the molar mass of each species present in multi species fluid.
|
inline |
Get the value of the molecular weight for an incompressible ideal gas (g/mol).
Definition at line 450 of file config_structure.inl.
|
inline |
Get final Outlet Pressure value for the ramp.
Definition at line 1198 of file config_structure.inl.
|
inline |
Get x-coordinate of the mesh motion origin.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 912 of file config_structure.inl.
|
inline |
Get y-coordinate of the mesh motion origin.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 914 of file config_structure.inl.
|
inline |
Get z-coordinate of the mesh motion origin.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 916 of file config_structure.inl.
|
inline |
Get if we should update the motion origin.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 972 of file config_structure.inl.
| SU2_MPI::Comm CConfig::GetMPICommunicator | ( | ) |
Get the MPI communicator of SU2.
Definition at line 152 of file config_structure.cpp.
|
inline |
Get the value of the constant viscosity.
Definition at line 876 of file config_structure.inl.
|
inline |
Get the value of the non-dimensional constant viscosity.
Definition at line 878 of file config_structure.inl.
|
inline |
Get the value of the reference viscosity for Sutherland model.
Definition at line 884 of file config_structure.inl.
|
inline |
Get the value of the non-dimensional reference viscosity for Sutherland model.
Definition at line 886 of file config_structure.inl.
|
inline |
Get the value of the reference S for Sutherland model.
Definition at line 892 of file config_structure.inl.
|
inline |
Get the value of the non-dimensional reference S for Sutherland model.
Definition at line 894 of file config_structure.inl.
|
inline |
Get the value of the reference temperature for Sutherland model.
Definition at line 888 of file config_structure.inl.
|
inline |
Get the value of the non-dimensional reference temperature for Sutherland model.
Definition at line 890 of file config_structure.inl.
| string CConfig::GetMultiInstance_FileName | ( | string | val_filename, |
| int | val_iInst | ||
| ) |
Append the instance index to the restart or the solution files.
Definition at line 7111 of file config_structure.cpp.
| string CConfig::GetMultiInstance_HistoryFileName | ( | string | val_filename, |
| int | val_iInst | ||
| ) |
Append the instance index to the restart or the solution files.
Definition at line 7124 of file config_structure.cpp.
| string CConfig::GetMultizone_FileName | ( | string | val_filename, |
| int | val_iZone | ||
| ) |
Append the zone index to the restart or the solution files.
Definition at line 7083 of file config_structure.cpp.
| string CConfig::GetMultizone_HistoryFileName | ( | string | val_filename, |
| int | val_iZone | ||
| ) |
Append the zone index to the restart or the solution files.
Definition at line 7097 of file config_structure.cpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 1070 of file config_structure.inl.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 1078 of file config_structure.inl.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 1080 of file config_structure.inl.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 1072 of file config_structure.inl.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 1076 of file config_structure.inl.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 1074 of file config_structure.inl.
|
inline |
Get the defintion of the nacelle location.
| [in] | val_index | - Index of the section. |
Definition at line 805 of file config_structure.inl.
|
inline |
number Turbomachinery blades computed using the pitch information.
Definition at line 1226 of file config_structure.inl.
| unsigned short CConfig::GetnDiatomics | ( | void | ) |
Retrieves the number of monatomic species in the multicomponent gas.
|
static |
Gets the number of dimensions in the mesh file.
| [in] | val_mesh_filename | - Name of the file with the grid information. |
| [in] | val_format | - Format of the file with the grid information. |
Definition at line 246 of file config_structure.cpp.
|
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Get the dimensionality of the electric field.
Definition at line 1837 of file config_structure.inl.
|
inline |
Get the number of design variables.
Definition at line 775 of file config_structure.inl.
|
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Get the number of design variables.
Definition at line 777 of file config_structure.inl.
|
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Get the number of different values for the elasticity modulus.
Definition at line 396 of file config_structure.inl.
|
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Get the number of different electric constants.
Definition at line 368 of file config_structure.inl.
|
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Get the number of different values for the modulus of the electric field.
Definition at line 1835 of file config_structure.inl.
| unsigned short* CConfig::GetnElStates | ( | void | ) |
Provides number electron states for calculating e_el.
|
inline |
Get the number of new elements added in the adaptation process.
Definition at line 1060 of file config_structure.inl.
|
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Get Newmark alpha parameter.
Definition at line 1827 of file config_structure.inl.
|
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Get Newmark delta parameter.
Definition at line 1829 of file config_structure.inl.
|
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Get the number of external iterations.
Definition at line 294 of file config_structure.inl.
|
inline |
Get the number of planes to fix in the I direction.
Definition at line 807 of file config_structure.inl.
|
inline |
Get the number of planes to fix in the J direction.
Definition at line 809 of file config_structure.inl.
|
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Get the number of planes to fix in the K direction.
Definition at line 811 of file config_structure.inl.
|
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Get the number of iterations to evaluate the parametric coordinates.
Definition at line 1735 of file config_structure.inl.
|
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Get the number of FFD boxes.
Definition at line 779 of file config_structure.inl.
|
inline |
Get the ID for the FEA region that we want to compute the gradient for using direct differentiation.
Definition at line 1873 of file config_structure.inl.
|
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Get the total number of types in Kind_Inc_Inlet list.
Definition at line 1172 of file config_structure.inl.
|
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Get the number of integration coefficients provided by the user.
Definition at line 1831 of file config_structure.inl.
|
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Get the number of fluid subiterations roblems.
Definition at line 1795 of file config_structure.inl.
|
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Get the number of subiterations while a ramp is applied.
Definition at line 1797 of file config_structure.inl.
|
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Get the number of time levels for time accurate local time stepping.
Definition at line 787 of file config_structure.inl.
|
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Get the number of sections.
Definition at line 1264 of file config_structure.inl.
|
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Get the total number of boundary markers.
Definition at line 1419 of file config_structure.inl.
|
inline |
Get the total number of boundary markers.
Definition at line 1421 of file config_structure.inl.
|
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Get the total number of boundary markers.
Definition at line 1393 of file config_structure.inl.
|
inline |
Get the total number of moving markers.
Definition at line 1415 of file config_structure.inl.
|
inline |
Get the total number of DV markers.
Definition at line 1409 of file config_structure.inl.
|
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Get the total number of boundary markers.
Definition at line 1399 of file config_structure.inl.
|
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Get the total number of boundary markers.
Definition at line 1397 of file config_structure.inl.
|
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Get the total number of boundary markers.
Definition at line 1403 of file config_structure.inl.
|
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Get the total number of heat flux markers.
Definition at line 1425 of file config_structure.inl.
|
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Get the total number of boundary markers.
Definition at line 1401 of file config_structure.inl.
|
inline |
Get the total number of boundary markers.
Definition at line 1395 of file config_structure.inl.
|
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number mixing plane interface specified from config file.
Definition at line 1234 of file config_structure.inl.
|
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Get the total number of monitoring markers.
Definition at line 1407 of file config_structure.inl.
|
inline |
Get the total number of moving markers.
Definition at line 1411 of file config_structure.inl.
|
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Get the total number of boundary markers.
Definition at line 1417 of file config_structure.inl.
|
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Get the total number of periodic markers.
Definition at line 1423 of file config_structure.inl.
|
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Get the total number of Python customizable markers.
Definition at line 1413 of file config_structure.inl.
|
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Get number of shroud markers.
Definition at line 1238 of file config_structure.inl.
|
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Get the total number of transpiration markers.
Definition at line 1405 of file config_structure.inl.
|
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number Turbomachinery performance option specified from config file.
Definition at line 1236 of file config_structure.inl.
|
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number Turbomachinery performance option specified from config file.
Definition at line 1242 of file config_structure.inl.
|
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Get the number of different values for the Material density.
Definition at line 400 of file config_structure.inl.
|
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Get the number of multigrid levels.
Definition at line 727 of file config_structure.inl.
| unsigned short CConfig::GetnMonatomics | ( | void | ) |
Retrieves the number of monatomic species in the multicomponent gas.
|
inline |
Get the total number of objectives in kind_objective list.
Definition at line 1427 of file config_structure.inl.
|
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Get the current number of non-physical nodes in the solution.
Definition at line 1785 of file config_structure.inl.
|
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Get the current number of non-physical reconstructions for 2nd-order upwinding.
Definition at line 1789 of file config_structure.inl.
|
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Get the total number of SEND_RECEIVE periodic transformations.
Definition at line 1621 of file config_structure.inl.
|
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Get the number of different values for the Poisson ratio.
Definition at line 398 of file config_structure.inl.
| unsigned short CConfig::GetnReactions | ( | void | ) |
Provides the number of chemical reactions in the chemistry model.
|
inline |
Get the number of Runge-Kutta steps.
Definition at line 785 of file config_structure.inl.
|
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set number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 1256 of file config_structure.inl.
|
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number span-wise sections to compute performance for turbomachinery.
Definition at line 1252 of file config_structure.inl.
|
inline |
number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 1246 of file config_structure.inl.
|
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Get the start up iterations using the fine grid, this works only for multigrid problems.
Definition at line 580 of file config_structure.inl.
|
inline |
Get the number time DOFs for ADER-DG.
Definition at line 791 of file config_structure.inl.
|
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Retrieves the number of periodic time instances for Harmonic Balance.
Definition at line 296 of file config_structure.inl.
|
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Get the number time integration points for ADER-DG.
Definition at line 795 of file config_structure.inl.
|
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Get the value of the non-dimensionalized engine turbulence intensity.
Definition at line 562 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream turbulence intensity.
Definition at line 560 of file config_structure.inl.
|
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Get the number of increments for an incremental load.
Definition at line 1863 of file config_structure.inl.
| unsigned short CConfig::GetnVar | ( | void | ) |
Provides the number of varaibles.
|
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Get the number of sections for computing internal volume.
Definition at line 1266 of file config_structure.inl.
|
static |
Gets the number of zones in the mesh file.
| [in] | val_mesh_filename | - Name of the file with the grid information. |
| [in] | val_format | - Format of the file with the grid information. |
| [in] | config | - Definition of the particular problem. |
Definition at line 164 of file config_structure.cpp.
|
inline |
Provides the number of varaibles.
Definition at line 278 of file config_structure.inl.
| string CConfig::GetObjFunc_Extension | ( | string | val_filename | ) |
Append the input filename string with the appropriate objective function extension.
| [in] | val_filename | - String value of the base filename. |
Definition at line 7137 of file config_structure.cpp.
|
inline |
Get the name of the file with the gradient of the objective function.
Definition at line 1479 of file config_structure.inl.
|
inline |
Get the name of the file with the gradient of the objective function.
Definition at line 1481 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 558 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 554 of file config_structure.inl.
|
inline |
Get the Harmonic Balance frequency pointer.
Definition at line 970 of file config_structure.inl.
|
inline |
Get the value of the reference angular velocity for non-dimensionalization.
Definition at line 532 of file config_structure.inl.
|
inline |
Get the bound for the line search.
Definition at line 1739 of file config_structure.inl.
|
inline |
Get the scale factor for the line search.
Definition at line 1741 of file config_structure.inl.
|
inline |
Value of the order of magnitude reduction of the residual.
Definition at line 1529 of file config_structure.inl.
|
inline |
Value of the order of magnitude reduction of the flow residual for BGS applications.
Definition at line 1891 of file config_structure.inl.
|
inline |
Value of the order of magnitude reduction of the flow residual for BGS applications.
Definition at line 1895 of file config_structure.inl.
|
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Value of the order of magnitude reduction of the residual for FSI applications.
Definition at line 1887 of file config_structure.inl.
| su2double CConfig::GetOutlet_Pressure | ( | string | val_index | ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7691 of file config_structure.cpp.
|
inline |
Get the format of the output solution.
Definition at line 1435 of file config_structure.inl.
|
inline |
Get a parameter of the particular design variable.
| [in] | val_dv | - Number of the design variable that we want to read. |
| [in] | val_param | - Index of the parameter that we want to read. |
Definition at line 765 of file config_structure.inl.
|
static |
Determine whether there are periodic BCs in the grid.
| [in] | val_mesh_filename | - Name of the file with the grid information. |
| [in] | val_format | - Format of the file with the grid information. |
| [in] | config | - Definition of the particular problem. |
Definition at line 344 of file config_structure.cpp.
|
inline |
Get the rotation center for a periodic transformation.
| [in] | val_index | - Index corresponding to the periodic transformation. |
Definition at line 1623 of file config_structure.inl.
| su2double * CConfig::GetPeriodicRotAngles | ( | string | val_marker | ) |
Angles of rotation for a rotational periodic boundary.
Definition at line 7399 of file config_structure.cpp.
|
inline |
Get the rotation angles for a periodic transformation.
| [in] | val_index | - Index corresponding to the periodic transformation. |
Definition at line 1629 of file config_structure.inl.
| su2double * CConfig::GetPeriodicRotCenter | ( | string | val_marker | ) |
Center of rotation for a rotational periodic boundary.
Definition at line 7392 of file config_structure.cpp.
|
inline |
Get the translation vector for a periodic transformation.
| [in] | val_index | - Index corresponding to the periodic transformation. |
Definition at line 1635 of file config_structure.inl.
| su2double * CConfig::GetPeriodicTranslation | ( | string | val_marker | ) |
Translation vector for a rotational periodic boundary.
Definition at line 7406 of file config_structure.cpp.
|
inline |
Get the pitching amplitude about the x-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 946 of file config_structure.inl.
|
inline |
Get the pitching amplitude about the y-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 948 of file config_structure.inl.
|
inline |
Get the pitching amplitude about the z-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 950 of file config_structure.inl.
|
inline |
Get the angular frequency of a mesh pitching about the x-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 940 of file config_structure.inl.
|
inline |
Get the angular frequency of a mesh pitching about the y-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 942 of file config_structure.inl.
|
inline |
Get the angular frequency of a mesh pitching about the z-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 944 of file config_structure.inl.
|
inline |
Get the pitching phase offset about the x-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 952 of file config_structure.inl.
|
inline |
Get the pitching phase offset about the y-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 954 of file config_structure.inl.
|
inline |
Get the pitching phase offset about the z-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 956 of file config_structure.inl.
|
inline |
Get index of the upper and lower horizontal plane.
| [in] | index | - 0 means upper surface, and 1 means lower surface. |
Definition at line 330 of file config_structure.inl.
|
inline |
Get information about writing sectional force files.
TRUE means that sectional force files will be written for specified markers. Definition at line 1677 of file config_structure.inl.
|
inline |
Get the plunging amplitude in the x-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 964 of file config_structure.inl.
|
inline |
Get the plunging amplitude in the y-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 966 of file config_structure.inl.
|
inline |
Get the plunging amplitude in the z-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 968 of file config_structure.inl.
|
inline |
Get the angular frequency of a mesh plunging in the x-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 958 of file config_structure.inl.
|
inline |
Get the angular frequency of a mesh plunging in the y-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 960 of file config_structure.inl.
|
inline |
Get the angular frequency of a mesh plunging in the z-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 962 of file config_structure.inl.
| su2double CConfig::GetPnormHeat | ( | void | ) |
Get the p-norm for heat-flux objective functions (adjoint problem).
|
inline |
Get the Poisson's ratio.
Definition at line 392 of file config_structure.inl.
|
inline |
Get information about the poisson solver condition.
TRUE if it is a poisson solver condition; otherwise FALSE. Definition at line 1585 of file config_structure.inl.
|
inline |
Value of the position of the Near Field (y coordinate for 2D, and z coordinate for 3D).
Definition at line 1541 of file config_structure.inl.
|
inline |
Get the value of the laminar Prandtl number.
Definition at line 504 of file config_structure.inl.
|
inline |
Get the value of the turbulent Prandtl number.
Definition at line 506 of file config_structure.inl.
|
inline |
Get the order of the predictor for FSI applications.
Definition at line 1859 of file config_structure.inl.
|
inline |
Get the value of the critical pressure.
Definition at line 866 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream pressure.
Definition at line 498 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream pressure.
Definition at line 536 of file config_structure.inl.
|
inline |
Get the value of the reference pressure for non-dimensionalization.
Definition at line 512 of file config_structure.inl.
|
inline |
Get the value of the thermodynamic pressure.
Definition at line 500 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized thermodynamic pressure.
Definition at line 538 of file config_structure.inl.
| su2double CConfig::GetPressureOut_BC | ( | ) |
Get the outlet pressure imposed as BC for internal flow.
Definition at line 7784 of file config_structure.cpp.
|
inline |
Decide whether it's necessary to read a reference geometry.
TRUE if it's necessary to read a reference geometry, FALSE otherwise. Definition at line 408 of file config_structure.inl.
|
inline |
Get the name of the file with the reference geometry of the structural problem.
Definition at line 416 of file config_structure.inl.
|
inline |
Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures).
TRUE if the mesh is matching, FALSE otherwise. Definition at line 1807 of file config_structure.inl.
|
inline |
Get QCR (SA-QCR2000).
Definition at line 1959 of file config_structure.inl.
|
inline |
Get the factor applied during quadrature of curved elements.
Definition at line 1917 of file config_structure.inl.
|
inline |
Get the factor applied during quadrature of straight elements.
Definition at line 1915 of file config_structure.inl.
|
inline |
Get the factor applied during time quadrature for ADER-DG.
Definition at line 1919 of file config_structure.inl.
|
inline |
Get the basis function radius to use for radial basis function interpolation for FSI.
Definition at line 1881 of file config_structure.inl.
|
inline |
Get option of whether to use polynomial terms in Radial Basis Function interpolation.
Definition at line 1879 of file config_structure.inl.
|
inline |
Check if the user wants to apply the load as a ramp.
TRUE means that the load is to be applied as a ramp. Definition at line 1845 of file config_structure.inl.
|
inline |
Get the maximum time of the ramp.
Definition at line 1847 of file config_structure.inl.
|
inline |
Check if the user wants to apply the load as a ramp.
TRUE means that the load is to be applied as a ramp. Definition at line 1849 of file config_structure.inl.
|
inline |
Get Outlet Pressure Ramp option.
Definition at line 1202 of file config_structure.inl.
|
inline |
Get coeff for Outlet Pressure Ramp.
Definition at line 1194 of file config_structure.inl.
|
inline |
Get Rotating Frame Ramp option.
Definition at line 1192 of file config_structure.inl.
|
inline |
Get coeff for Rotating Frame Ramp.
Definition at line 1190 of file config_structure.inl.
|
inline |
Flag for whether binary SU2 native restart files are read.
TRUE then the code will load binary restart files. Definition at line 1290 of file config_structure.inl.
|
inline |
Get the kind of incompressible non-dimensionalization.
Definition at line 286 of file config_structure.inl.
|
inline |
Get the kind of non-dimensionalization.
Definition at line 284 of file config_structure.inl.
|
inline |
Get the reference area for non dimensional coefficient computation. If the value from the is 0 then, the code will compute the reference area using the projection of the shape into the z plane (3D) or the x plane (2D).
Definition at line 356 of file config_structure.inl.
|
inline |
Get the reference element length for computing the slope limiting epsilon.
Definition at line 420 of file config_structure.inl.
|
inline |
Decide whether it's necessary to read a reference geometry.
TRUE if it's necessary to read a reference geometry, FALSE otherwise. Definition at line 384 of file config_structure.inl.
|
inline |
Get the name of the file with the reference geometry of the structural problem.
Definition at line 386 of file config_structure.inl.
|
inline |
Get the format of the reference geometry file.
Definition at line 388 of file config_structure.inl.
|
inline |
Get the penalty weight value for the objective function.
Definition at line 1855 of file config_structure.inl.
|
inline |
Get the reference length for computing moment (the default value is 1).
Definition at line 418 of file config_structure.inl.
|
inline |
Get the values for the reference node displacement.
| [in] | val_coeff | - Index of the displacement. |
Definition at line 380 of file config_structure.inl.
|
inline |
Get the ID of the reference node.
Definition at line 378 of file config_structure.inl.
|
inline |
Get the penalty weight value for the objective function.
Definition at line 382 of file config_structure.inl.
|
inline |
Get reference origin for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 582 of file config_structure.inl.
|
inline |
Get reference origin x-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 591 of file config_structure.inl.
|
inline |
Get reference origin y-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 593 of file config_structure.inl.
|
inline |
Get reference origin z-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 595 of file config_structure.inl.
|
inline |
Get the reference coefficient for detecting sharp edges.
Definition at line 422 of file config_structure.inl.
| su2double* CConfig::GetRefTemperature | ( | void | ) |
Provides the thermodynamic reference temperatures from the JANAF tables.
|
inline |
Get the relaxation coefficient of the linear solver for the implicit formulation.
Definition at line 1004 of file config_structure.inl.
|
inline |
Get the relaxation coefficient of the CHT coupling.
Definition at line 1008 of file config_structure.inl.
|
inline |
Get the relaxation coefficient of the linear solver for the implicit formulation.
Definition at line 1002 of file config_structure.inl.
|
inline |
Get the relaxation coefficient of the linear solver for the implicit formulation.
Definition at line 1006 of file config_structure.inl.
|
inline |
Get the relaxation method chosen for the simulation.
Definition at line 1885 of file config_structure.inl.
|
inline |
Get information about element reorientation.
TRUE means that elements can be reoriented if suspected unhealthy Definition at line 324 of file config_structure.inl.
|
inline |
Get the criteria for structural residual (relative/absolute).
Definition at line 1491 of file config_structure.inl.
|
inline |
Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale).
Definition at line 1903 of file config_structure.inl.
|
inline |
Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale).
Definition at line 1901 of file config_structure.inl.
|
inline |
Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale).
Definition at line 1899 of file config_structure.inl.
| string CConfig::GetResidual_FileName | ( | void | ) |
Get the name of the file with the residual of the problem.
|
inline |
Get functional that is going to be used to evaluate the residual flow convergence.
Definition at line 1493 of file config_structure.inl.
|
inline |
Provides the restart information.
TRUE then the code will use the solution as restart. Definition at line 1286 of file config_structure.inl.
|
inline |
Get the name of the restart file for the structural adjoint variables.
Definition at line 1475 of file config_structure.inl.
|
inline |
Get the name of the restart file for the adjoint variables (drag objective function).
Definition at line 1471 of file config_structure.inl.
|
inline |
Set the sum of the bandwidth for writing binary restarts (to be averaged later).
Definition at line 1949 of file config_structure.inl.
|
inline |
Get the name of the restart file for the structural variables.
Definition at line 1473 of file config_structure.inl.
|
inline |
For some problems like adjoint or the linearized equations it is necessary to restart the flow solution.
TRUE then the code will restart the flow solution. Definition at line 1292 of file config_structure.inl.
|
inline |
Get the name of the restart file for the flow variables.
Definition at line 1467 of file config_structure.inl.
|
inline |
Get the name of the restart file for the heat variables.
Definition at line 1469 of file config_structure.inl.
|
inline |
Get the Reynolds number. Dimensionless number that gives a measure of the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow condition.
Definition at line 611 of file config_structure.inl.
| su2double * CConfig::GetRiemann_FlowDir | ( | string | val_marker | ) |
Get the Flowdir at Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 7719 of file config_structure.cpp.
|
inline |
Get the kind of Riemann solver for the DG method (FEM flow solver).
Definition at line 1913 of file config_structure.inl.
| su2double CConfig::GetRiemann_Var1 | ( | string | val_marker | ) |
Get the var 1 at Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 7705 of file config_structure.cpp.
| su2double CConfig::GetRiemann_Var2 | ( | string | val_marker | ) |
Get the var 2 at Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 7712 of file config_structure.cpp.
|
inline |
Get the relaxation coefficient of the linear solver for the implicit formulation.
Definition at line 1010 of file config_structure.inl.
|
inline |
Get information about the rotational frame.
TRUE if there is a rotational frame; otherwise FALSE. Definition at line 1579 of file config_structure.inl.
|
inline |
Get the angular velocity of the mesh about the x-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 930 of file config_structure.inl.
|
inline |
Get the angular velocity of the mesh about the y-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 932 of file config_structure.inl.
|
inline |
Get the angular velocity of the mesh about the z-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 934 of file config_structure.inl.
| su2double* CConfig::GetRotationModes | ( | void | ) |
Provides the number of rotational modes of energy storage.
| su2double* CConfig::GetRxnTcb_a | ( | void | ) |
Provides the rate controlling temperature exponents for chemistry.
| su2double* CConfig::GetRxnTcb_b | ( | void | ) |
Provides the rate controlling temperature exponents for chemistry.
| su2double* CConfig::GetRxnTcf_a | ( | void | ) |
Provides the rate controlling temperature exponents for chemistry.
| su2double* CConfig::GetRxnTcf_b | ( | void | ) |
Provides the rate controlling temperature exponents for chemistry.
|
inline |
Get the value of the non-dimensionalized actuator disk turbulence intensity.
Definition at line 564 of file config_structure.inl.
|
inline |
Get the wing semi span.
Definition at line 1012 of file config_structure.inl.
|
inline |
Provides information about if the sharp edges are going to be removed from the sensitivity.
FALSE means that the sharp edges will be removed from the sensitivity. Definition at line 1615 of file config_structure.inl.
|
inline |
Check if the user wants to apply the load as a ramp.
TRUE means that the load is to be applied as a ramp. Definition at line 1851 of file config_structure.inl.
|
inline |
Function to make available the matrix size in vectorization in order to optimize the gemm performance.
Definition at line 1923 of file config_structure.inl.
|
inline |
Get information about there is a smoothing of the grid coordinates.
TRUE if there is smoothing of the grid coordinates; otherwise FALSE. Definition at line 1597 of file config_structure.inl.
|
inline |
Get the name of the file with the solution of the adjoint structural problem.
Definition at line 1451 of file config_structure.inl.
|
inline |
Get the name of the file with the solution of the adjoint flow problem with drag objective function.
Definition at line 1447 of file config_structure.inl.
|
inline |
Get the name of the file with the solution of the structural problem.
Definition at line 1449 of file config_structure.inl.
|
inline |
Get the name of the file with the solution of the flow problem.
Definition at line 1445 of file config_structure.inl.
|
inline |
Verify if there is mixing plane interface specified from config file.
Definition at line 1224 of file config_structure.inl.
|
inline |
Get the value of specific heat at constant pressure.
Definition at line 452 of file config_structure.inl.
|
inline |
Get the value of the specific heat for solids.
Definition at line 454 of file config_structure.inl.
|
inline |
Get the non-dimensional value of specific heat at constant pressure.
Definition at line 456 of file config_structure.inl.
|
inline |
Get the value of specific heat at constant volume.
Definition at line 458 of file config_structure.inl.
|
inline |
Get the non-dimensional value of specific heat at constant volume.
Definition at line 460 of file config_structure.inl.
| su2double CConfig::GetSpline | ( | vector< su2double > & | xa, |
| vector< su2double > & | ya, | ||
| vector< su2double > & | y2a, | ||
| unsigned long | n, | ||
| su2double | x | ||
| ) |
Given the arrays xa[1..n] and ya[1..n], which tabulate a function (with the xai’s in order), and given the array y2a[1..n], which is the output from spline above, and given a value of x, this routine returns a cubic-spline interpolated value y. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++.
Definition at line 8457 of file config_structure.cpp.
|
inline |
Get the number of iterations that are not considered in the convergence criteria.
Definition at line 1501 of file config_structure.inl.
|
inline |
Get the value of the limits for the sections.
Definition at line 438 of file config_structure.inl.
|
inline |
Identifies if we want to restart from a steady or an unsteady solution.
TRUE if we restart from steady state solution, FALSE otherwise. Definition at line 1811 of file config_structure.inl.
|
inline |
Get the name of the file with the structure variables.
Definition at line 1455 of file config_structure.inl.
|
inline |
Divide the rectbles and hexahedron.
TRUE if the elements must be divided; otherwise FALSE. Definition at line 1517 of file config_structure.inl.
|
inline |
Get the the coordinates where of the box where a subsonic region is imposed.
Definition at line 340 of file config_structure.inl.
|
inline |
Get the the coordinates where of the box where a subsonic region is imposed.
Definition at line 342 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 214 of file config_structure.inl.
|
inline |
Get the density at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 194 of file config_structure.inl.
|
inline |
Get the enthalpy at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 196 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 216 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 218 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 220 of file config_structure.inl.
|
inline |
Get the mach number at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 188 of file config_structure.inl.
|
inline |
Get the massflow at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 186 of file config_structure.inl.
|
inline |
Get the momentum distortion at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
Definition at line 206 of file config_structure.inl.
|
inline |
Get the normal velocity at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 198 of file config_structure.inl.
|
inline |
Get the pressure at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 192 of file config_structure.inl.
|
inline |
Get the pressure drop between two surfaces.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 212 of file config_structure.inl.
|
inline |
Get the secondary flow strength at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
Definition at line 202 of file config_structure.inl.
|
inline |
Get the relative secondary flow strength at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
Definition at line 204 of file config_structure.inl.
|
inline |
Get the temperature at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 190 of file config_structure.inl.
|
inline |
Get the total pressure at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 210 of file config_structure.inl.
|
inline |
Get the total temperature at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 208 of file config_structure.inl.
|
inline |
Get the streamwise flow uniformity at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
Definition at line 200 of file config_structure.inl.
|
inline |
Get the name of the file with the surface information for the adjoint problem.
Definition at line 1485 of file config_structure.inl.
|
inline |
Get the name of the file with the surface information for the flow problem.
Definition at line 1483 of file config_structure.inl.
|
inline |
Get the name of the file with the structure variables.
Definition at line 1463 of file config_structure.inl.
|
inline |
Get the name of the file with the surface sensitivity (discrete adjoint).
Definition at line 1487 of file config_structure.inl.
|
inline |
Get the name of the file with the structure variables.
Definition at line 1457 of file config_structure.inl.
|
inline |
Governing equations of the flow (it can be different from the run time equation).
| [in] | val_zone | - Zone where the soler is applied. |
Definition at line 852 of file config_structure.inl.
|
inline |
Get the FFD Tag of a particular FFD box.
| [in] | val_ffd | - Number of the FFD box that we want to read. |
Definition at line 773 of file config_structure.inl.
|
inline |
Get the value specified for the target CL.
Definition at line 1757 of file config_structure.inl.
|
inline |
Get the value of the critical temperature.
Definition at line 868 of file config_structure.inl.
|
inline |
Get the value of the frestream temperature.
Definition at line 484 of file config_structure.inl.
|
inline |
Get the temperature in solids at freestream conditions.
Definition at line 362 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream temperature.
Definition at line 540 of file config_structure.inl.
|
inline |
Get the value of the reference temperature for non-dimensionalization.
Definition at line 514 of file config_structure.inl.
|
inline |
Get the value of the frestream vibrational-electronic temperature.
Definition at line 502 of file config_structure.inl.
|
inline |
Get the thermal expansion coefficient.
Definition at line 462 of file config_structure.inl.
|
inline |
Get the non-dim. thermal expansion coefficient.
Definition at line 464 of file config_structure.inl.
|
inline |
Get the value of the thermal conductivity for solids.
Definition at line 508 of file config_structure.inl.
|
inline |
Get the wave speed.
Definition at line 358 of file config_structure.inl.
|
inline |
Get the value of the thermal diffusivity for solids.
Definition at line 360 of file config_structure.inl.
|
inline |
Function to make available the multiplication factor theta of the symmetrizing terms in the DG discretization of the viscous terms.
Definition at line 1921 of file config_structure.inl.
|
inline |
Get the value of the reference time for non-dimensionalization.
Definition at line 522 of file config_structure.inl.
|
inline |
Get the location of the time DOFs for ADER-DG on the interval [-1..1].
Definition at line 793 of file config_structure.inl.
|
inline |
Get the location of the time integration points for ADER-DG on the interval [-1..1].
Definition at line 797 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 556 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 552 of file config_structure.inl.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 1817 of file config_structure.inl.
|
inline |
If we are performing an unsteady simulation, this is the value of max physical time for which we run the simulation.
Definition at line 1515 of file config_structure.inl.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 1507 of file config_structure.inl.
|
inline |
Get the penalty weight value for the objective function.
Definition at line 1857 of file config_structure.inl.
| su2double CConfig::GetTotalPressureIn_BC | ( | ) |
Get the inlet total pressure imposed as BC for internal flow.
Definition at line 7815 of file config_structure.cpp.
| su2double CConfig::GetTotalTemperatureIn_BC | ( | ) |
Get the inlet total temperature imposed as BC for internal flow.
Definition at line 7834 of file config_structure.cpp.
|
inline |
Get the translational velocity of the mesh in the x-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 924 of file config_structure.inl.
|
inline |
Get the translational velocity of the mesh in the y-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 926 of file config_structure.inl.
|
inline |
Get the translational velocity of the mesh in the z-direction.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
Definition at line 928 of file config_structure.inl.
|
inline |
Provides the transpiration objective information.
TRUE then the code will add the jet blowing coefficient to the objective. Definition at line 741 of file config_structure.inl.
|
inline |
Get the name of file containing all transpirations.
| void CConfig::GetTranspirationParams | ( | string | val_marker, |
| su2double & | x0, | ||
| su2double & | x1, | ||
| su2double & | x2, | ||
| su2double & | x3, | ||
| su2double & | y0, | ||
| su2double & | y1, | ||
| su2double & | y2, | ||
| su2double & | y3, | ||
| su2double & | eps0, | ||
| su2double & | eps1, | ||
| su2double & | eps2, | ||
| su2double & | eps3 | ||
| ) |
Get the wall transpiration parameters.
| [in] | val_index | - Index corresponding to the transpiration boundary. |
Definition at line 7994 of file config_structure.cpp.
|
inline |
Obtain the marker of a transpiration DV.
| [in] | val_dv | - Number of the design variable that we want to read. |
Definition at line 739 of file config_structure.inl.
|
inline |
Get the value of the turbulent to laminar viscosity ratio.
Definition at line 574 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream turbulence intensity.
Definition at line 572 of file config_structure.inl.
|
inline |
Get the starting direct iteration number for the unsteady adjoint (reverse time integration).
Definition at line 322 of file config_structure.inl.
|
inline |
Get the Courant Friedrich Levi number for unsteady simulations.
Definition at line 761 of file config_structure.inl.
|
inline |
Get the number of internal iterations.
Definition at line 316 of file config_structure.inl.
|
inline |
Get the restart iteration number for unsteady simulations.
Definition at line 320 of file config_structure.inl.
| string CConfig::GetUnsteady_FileName | ( | string | val_filename, |
| int | val_iter | ||
| ) |
Augment the input filename with the iteration number for an unsteady file.
| [in] | val_filename | - String value of the base filename. |
| [in] | val_iter | - Unsteady iteration number or time instance. |
Definition at line 7055 of file config_structure.cpp.
|
inline |
Provides information about the time integration, and change the write in the output files information about the iteration.
Definition at line 1284 of file config_structure.inl.
|
inline |
Get the value of iterations to re-evaluate the angle of attack.
Definition at line 1767 of file config_structure.inl.
|
inline |
Get information about whether to update the AoA for fixed lift mode.
TRUE if we should update the AoA for fixed lift mode; otherwise FALSE. Definition at line 1771 of file config_structure.inl.
|
inline |
Get the value of iterations to re-evaluate the angle of attack.
Definition at line 1777 of file config_structure.inl.
|
inline |
Get information about whether to update the AoA for fixed lift mode.
TRUE if we should update the AoA for fixed lift mode; otherwise FALSE. Definition at line 1773 of file config_structure.inl.
|
inline |
Function to make available whether or not the lumped mass matrix must be used for steady computations.
Definition at line 1927 of file config_structure.inl.
|
inline |
Get the vector of the dimensionalized freestream velocity.
Definition at line 546 of file config_structure.inl.
|
inline |
Get the vector of the non-dimensionalized freestream velocity.
Definition at line 544 of file config_structure.inl.
|
inline |
Get the value of the reference velocity for non-dimensionalization.
Definition at line 518 of file config_structure.inl.
|
inline |
Get the value of limiter coefficient.
Definition at line 605 of file config_structure.inl.
|
inline |
Get the value of the frestream temperature.
Definition at line 488 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 550 of file config_structure.inl.
|
inline |
Get the value of the reference viscosity for non-dimensionalization.
Definition at line 524 of file config_structure.inl.
|
inline |
Determines if problem is viscous.
Definition at line 292 of file config_structure.inl.
|
inline |
Get the node number of the CV to visualize.
Definition at line 1745 of file config_structure.inl.
|
inline |
Creates a teot file to visualize the surface deformation deformation made by the DEF software.
TRUE if the deformation is going to be plotted; otherwise FALSE. Definition at line 1054 of file config_structure.inl.
|
inline |
Creates a tecplot file to visualize the volume deformation deformation made by the DEF software.
TRUE if the deformation is going to be plotted; otherwise FALSE. Definition at line 1052 of file config_structure.inl.
|
inline |
Get the name of the file with the volume sensitivity (discrete adjoint).
Definition at line 1489 of file config_structure.inl.
|
inline |
Get information about whether to use wall functions.
TRUE if wall functions are on; otherwise FALSE. Definition at line 1747 of file config_structure.inl.
| su2double CConfig::GetWall_HeatFlux | ( | string | val_index | ) |
Get the wall heat flux on a constant heat flux boundary.
| [in] | val_index | - Index corresponding to the constant heat flux boundary. |
Definition at line 7972 of file config_structure.cpp.
| su2double * CConfig::GetWallFunction_DoubleInfo | ( | string | val_marker | ) |
Get the additional double info for the wall function treatment for the given boundary marker.
| [in] | val_marker | - String of the viscous wall marker. |
Definition at line 8073 of file config_structure.cpp.
| unsigned short * CConfig::GetWallFunction_IntInfo | ( | string | val_marker | ) |
Get the additional integer info for the wall function treatment for the given boundary marker.
| [in] | val_marker | - String of the viscous wall marker. |
Definition at line 8060 of file config_structure.cpp.
| unsigned short CConfig::GetWallFunction_Treatment | ( | string | val_marker | ) |
Get the wall function treatment for the given boundary marker.
| [in] | val_marker | - String of the viscous wall marker. |
Definition at line 8047 of file config_structure.cpp.
|
inline |
Get the value of wall temperature.
Definition at line 480 of file config_structure.inl.
|
inline |
Get the heat equation.
Definition at line 1931 of file config_structure.inl.
|
inline |
Get the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.
Definition at line 1276 of file config_structure.inl.
|
inline |
Value of the weight of the drag coefficient in the Sonic Boom optimization.
Definition at line 1543 of file config_structure.inl.
|
inline |
Get the weights of the time integration points for ADER-DG.
Definition at line 799 of file config_structure.inl.
|
inline |
Get information about the wind gust.
TRUE if there is a wind gust; otherwise FALSE. Definition at line 1717 of file config_structure.inl.
|
inline |
Write convergence file for FSI problems.
FALSE means no file is written. Definition at line 1617 of file config_structure.inl.
|
inline |
Flag for whether binary SU2 native restart files are written.
TRUE then the code will output binary restart files. Definition at line 1288 of file config_structure.inl.
|
inline |
Get the frequency for writing the convergence file.
Definition at line 838 of file config_structure.inl.
|
inline |
Get the frequency for writing the convergence file in Dual Time.
Definition at line 842 of file config_structure.inl.
|
inline |
Get information about writing a binary coordinates file.
TRUE means that a binary coordinates file will be written. Definition at line 1657 of file config_structure.inl.
|
inline |
Get information about writing a surface comma-separated values (CSV) solution file.
TRUE means that a surface comma-separated values (CSV) solution file will be written. Definition at line 1655 of file config_structure.inl.
|
inline |
Get information about writing dynamic structural analysis headers and file extensions.
TRUE means that dynamic structural analysis solution files will be written. Definition at line 1825 of file config_structure.inl.
|
inline |
Get information about writing rind layers to the solution files.
TRUE means that rind layers will be written to the solution file. Definition at line 1667 of file config_structure.inl.
|
inline |
Get information about writing a template inlet profile file.
TRUE means that a template inlet profile file will be written. Definition at line 1671 of file config_structure.inl.
|
inline |
Get information about writing residuals to volume solution file.
TRUE means that residuals will be written to the solution file. Definition at line 1661 of file config_structure.inl.
|
inline |
Get information about writing output files.
TRUE means that output files will be written. Definition at line 1649 of file config_structure.inl.
|
inline |
Get information about writing the performance summary at the end of a calculation.
TRUE means that the performance summary will be written at the end of a calculation. Definition at line 1669 of file config_structure.inl.
|
inline |
Get information about writing residuals to volume solution file.
TRUE means that residuals will be written to the solution file. Definition at line 1659 of file config_structure.inl.
|
inline |
Get information about writing residuals to volume solution file.
TRUE means that residuals will be written to the solution file. Definition at line 1665 of file config_structure.inl.
|
inline |
Get information about writing a 1D slice of a 2D cartesian solution.
TRUE means that a 1D slice of a 2D cartesian solution will be written. Definition at line 1675 of file config_structure.inl.
|
inline |
Get the frequency for writing the solution file.
Definition at line 834 of file config_structure.inl.
|
inline |
Get the frequency for writing the solution file in Dual Time.
Definition at line 836 of file config_structure.inl.
|
inline |
Get information about writing a surface solution file.
TRUE means that a surface solution file will be written. Definition at line 1653 of file config_structure.inl.
|
inline |
Get the frequency for writing the surface solution file in Dual Time.
Definition at line 1951 of file config_structure.inl.
|
inline |
Write solution at each surface.
TRUE means that the solution at each surface will be written. Definition at line 1663 of file config_structure.inl.
|
inline |
Get information about writing unsteady headers and file extensions.
TRUE means that unsteady solution files will be written. Definition at line 844 of file config_structure.inl.
|
inline |
Get information about writing a volume solution file.
TRUE means that a volume solution file will be written. Definition at line 1651 of file config_structure.inl.
|
inline |
Get information about the Low Mach Correction.
TRUE if we are using low Mach correction; otherwise FALSE. Definition at line 1589 of file config_structure.inl.
|
inline |
Get information about the Low Mach Preconditioning.
TRUE if we are using low Mach preconditioner; otherwise FALSE. Definition at line 1587 of file config_structure.inl.
|
inline |
Set the boolean addCrossTerm to true or false.
Definition at line 412 of file config_structure.inl.
|
inline |
Set the values for the electric field modulus.
| [in] | val_coeff | - Index of the electric field. |
| [in] | val_el_field | - Value of the electric field. |
Definition at line 1841 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 162 of file config_structure.inl.
| void CConfig::SetActDisk_BCThrust | ( | string | val_marker, |
| su2double | val_actdisk_bcthrust | ||
| ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7487 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 156 of file config_structure.inl.
| void CConfig::SetActDisk_BCThrust_Old | ( | string | val_marker, |
| su2double | val_actdisk_bcthrust_old | ||
| ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7495 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 158 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 98 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 144 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 106 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 160 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 104 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 102 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 154 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 100 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 150 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 152 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 146 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 148 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 240 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 248 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 242 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 234 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 238 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 164 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 244 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 236 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 246 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 256 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 254 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 264 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 258 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 250 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 260 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 252 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 262 of file config_structure.inl.
|
inline |
Value of Aeroelastic solution coordinate at time n from time n+1.
Definition at line 1699 of file config_structure.inl.
|
inline |
Value of Aeroelastic solution coordinate at time n-1 from time n.
Definition at line 1695 of file config_structure.inl.
|
inline |
Value of Aeroelastic solution coordinate at time n+1.
Definition at line 1685 of file config_structure.inl.
|
inline |
Value of pitching coordinate.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val | - value of pitching coordinate. |
Definition at line 1693 of file config_structure.inl.
|
inline |
Value of plunging coordinate.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val | - value of plunging coordinate. |
Definition at line 1691 of file config_structure.inl.
|
inline |
Set the angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 709 of file config_structure.inl.
|
inline |
Set the off set angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 711 of file config_structure.inl.
|
inline |
Set the angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 715 of file config_structure.inl.
|
inline |
Set the angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 717 of file config_structure.inl.
|
inline |
Set the off set sideslip angle.
| [in] | val_AoA | - Value of the off set sideslip angle. |
Definition at line 713 of file config_structure.inl.
|
inline |
Get the Courant Friedrich Levi number for each grid.
| [in] | val_mesh | - Index of the mesh were the CFL is applied. |
Definition at line 759 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 701 of file config_structure.inl.
| void CConfig::SetConfig_Parsing | ( | char | case_filename[MAX_STRING_SIZE] | ) |
Set the config file parsing.
Definition at line 2282 of file config_structure.cpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1553 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1567 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1561 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1563 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1555 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1557 of file config_structure.inl.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 1559 of file config_structure.inl.
|
inline |
Set the value of the unsteadty time step using the CFL number.
| [in] | val_delta_unsttimend | - Value of the unsteady time step using CFL number. |
Definition at line 1513 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 625 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 623 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 677 of file config_structure.inl.
| void CConfig::SetdNetThrust_dBCThrust | ( | su2double | val_dnetthrust_dbcthrust | ) |
Value of the weight of the CD, CL, CM optimization.
|
inline |
Set the value of the domain volume computed on the finest grid.
| [in] | val_volume | - Value of the domain volume computed on the finest grid. |
Definition at line 430 of file config_structure.inl.
|
inline |
Set the value of the design variable step, we use this value in design problems.
| [in] | val_dv | - Number of the design variable that we want to read. |
| [in] | val | - Value of the design variable. |
Definition at line 1527 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 661 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 659 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 703 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_area | - Exhaust power. |
Definition at line 96 of file config_structure.inl.
|
inline |
Set the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_force | - Exhaust power. |
Definition at line 88 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_grossthrust | - Exhaust power. |
Definition at line 94 of file config_structure.inl.
|
inline |
Set the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_mach | - Exhaust power. |
Definition at line 86 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_netthrust | - Exhaust power. |
Definition at line 92 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_imarker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_power | - Exhaust power. |
Definition at line 90 of file config_structure.inl.
|
inline |
Set boolean for using Persson's shock capturing method in Euler flow DG-FEM.
| [in] | val_EulerPersson | - Boolean for using Persson's shock capturing method in Euler flow DG-FEM |
Definition at line 1869 of file config_structure.inl.
|
inline |
Set the force balance at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_force | - Exhaust force balance. |
Definition at line 82 of file config_structure.inl.
|
inline |
Set the gross thrust at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_grossthrust | - Exhaust gross thrust temperature. |
Definition at line 80 of file config_structure.inl.
|
inline |
Set the back pressure (static) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_temp | - Exhaust static temperature. |
Definition at line 74 of file config_structure.inl.
|
inline |
Set the power at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_power | - Exhaust power. |
Definition at line 84 of file config_structure.inl.
|
inline |
Set the back pressure (static) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_pressure | - Exhaust static pressure. |
Definition at line 70 of file config_structure.inl.
|
inline |
Set the temperature (static) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_temp | - Exhaust static temperature. |
Definition at line 72 of file config_structure.inl.
|
inline |
Set the back pressure (total) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_totalpressure | - Exhaust total pressure. |
Definition at line 76 of file config_structure.inl.
|
inline |
Set the total temperature at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_totaltemp | - Exhaust total temperature. |
Definition at line 78 of file config_structure.inl.
|
inline |
Set the current external iteration number.
| [in] | val_iter | - Current external iteration number. |
Definition at line 300 of file config_structure.inl.
|
inline |
Set the current external iteration number.
| [in] | val_iter | - Current external iteration number. |
Definition at line 302 of file config_structure.inl.
|
inline |
Set the finest mesh in a multigrid strategy.
| [in] | val_finestmesh | - Index of the finest grid. |
Definition at line 733 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 685 of file config_structure.inl.
| void CConfig::SetFreeStreamTurboNormal | ( | su2double * | turboNormal | ) |
Set freestream turbonormal for initializing solution.
Definition at line 8908 of file config_structure.cpp.
|
inline |
Set the Froude number for free surface problems.
Definition at line 665 of file config_structure.inl.
|
inline |
Set the current FSI iteration number.
| [in] | val_iter | - Current FSI iteration number. |
Definition at line 304 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 689 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 687 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 637 of file config_structure.inl.
| void CConfig::SetGiles_Var1 | ( | su2double | newVar1, |
| string | val_marker | ||
| ) |
Set the var 1 for Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 7741 of file config_structure.cpp.
| void CConfig::SetGlobalParam | ( | unsigned short | val_solver, |
| unsigned short | val_system, | ||
| unsigned long | val_extiter | ||
| ) |
Set the global parameters of each simulation for each runtime system.
| [in] | val_solver | - Solver of the simulation. |
| [in] | val_system | - Runtime system that we are solving. |
Definition at line 7239 of file config_structure.cpp.
|
inline |
Set the heat flux reference value.
Definition at line 697 of file config_structure.inl.
|
inline |
Set the ofstream of the history file for the current zone.
Definition at line 1965 of file config_structure.inl.
|
inline |
Set the current instance.
| [in] | iInst | - current instance identifier. |
Definition at line 1823 of file config_structure.inl.
| void CConfig::SetIncInlet_BC | ( | su2double | val_in | ) |
Set the inlet velocity or pressure imposed as BC for incompressible flow.
| [in] | val_in | - New value of the inlet velocity or pressure. |
Definition at line 7907 of file config_structure.cpp.
| void CConfig::SetIncPressureOut_BC | ( | su2double | val_pressure | ) |
Set the outlet pressure imposed as BC for incompressible flow.
| [in] | val_pressure | - New value of the outlet pressure. |
Definition at line 7950 of file config_structure.cpp.
| void CConfig::SetIncTemperature_BC | ( | su2double | val_temperature | ) |
Set the inlet temperature imposed as BC for incompressible flow.
| [in] | val_temperature | - New value of the inlet temperature. |
Definition at line 7929 of file config_structure.cpp.
|
inline |
Set the force balance at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_force | - Fan face force. |
Definition at line 64 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 48 of file config_structure.inl.
|
inline |
Set the massflow at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_massflow | - Massflow. |
Definition at line 52 of file config_structure.inl.
|
inline |
Set the power at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_force | - Power. |
Definition at line 66 of file config_structure.inl.
|
inline |
Set the fan face static pressure at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_pressure | - Fan face static pressure. |
Definition at line 50 of file config_structure.inl.
|
inline |
Set the ram drag temperature at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_ramdrag | - Ram drag value. |
Definition at line 62 of file config_structure.inl.
|
inline |
Set the reverse flow at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_reversemassflow | - reverse flow. |
Definition at line 54 of file config_structure.inl.
|
inline |
Set the fan face static temperature at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_pressure | - Fan face static temperature. |
Definition at line 58 of file config_structure.inl.
|
inline |
Set the fan face total pressure at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_totalpressure | - Fan face total pressure. |
Definition at line 56 of file config_structure.inl.
|
inline |
Set the fan face total temperature at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_totaltemperature | - Fan face total temperature. |
Definition at line 60 of file config_structure.inl.
|
inline |
Get the value of the non-dimensionalized actuator disk turbulence intensity.
Definition at line 568 of file config_structure.inl.
| void CConfig::SetInlet_Ptotal | ( | su2double | val_pressure, |
| string | val_marker | ||
| ) |
Set the total pressure at an inlet boundary.
| [in] | val_pressure | - Pressure value at the inlet boundary. |
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 7656 of file config_structure.cpp.
|
inline |
Set the current internal iteration number.
| [in] | val_iter | - Current external iteration number. |
Definition at line 306 of file config_structure.inl.
|
inline |
Set the kind of preconditioner for the implicit solver.
Definition at line 1024 of file config_structure.inl.
|
inline |
Set the kind of mixing process for averaging quantities at the boundaries.
Definition at line 1186 of file config_structure.inl.
| void CConfig::SetKind_ConvNumScheme | ( | unsigned short | val_kind_convnumscheme, |
| unsigned short | val_kind_centered, | ||
| unsigned short | val_kind_upwind, | ||
| unsigned short | val_kind_slopelimit, | ||
| bool | val_muscl, | ||
| unsigned short | val_kind_fem | ||
| ) |
Set the parameters of the convective numerical scheme.
| [in] | val_kind_convnumscheme | - Center or upwind scheme. |
| [in] | val_kind_centered | - If centered scheme, kind of centered scheme (JST, etc.). |
| [in] | val_kind_upwind | - If upwind scheme, kind of upwind scheme (Roe, etc.). |
| [in] | val_kind_slopelimit | - If upwind scheme, kind of slope limit. |
| [in] | val_muscl | - Define if we apply a MUSCL scheme or not. |
| [in] | val_kind_fem | - If FEM, what kind of FEM discretization. |
Definition at line 7225 of file config_structure.cpp.
|
inline |
Set the kind of preconditioner for the implicit solver.
Definition at line 984 of file config_structure.inl.
|
inline |
Set the type of dynamic mesh motion.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
| [in] | motion_Type | - Specify motion type. |
Definition at line 908 of file config_structure.inl.
|
inline |
Set the kind of preconditioner for the implicit solver.
Definition at line 988 of file config_structure.inl.
|
inline |
Set the kind of mixing process for averaging quantities at the boundaries.
Definition at line 1188 of file config_structure.inl.
|
inline |
Governing equations of the flow (it can be different from the run time equation).
| [in] | val_zone | - Zone where the soler is applied. |
Definition at line 848 of file config_structure.inl.
|
inline |
Get the kind of SU2 software component.
Definition at line 288 of file config_structure.inl.
|
inline |
Set the kind of time integration scheme.
| [in] | val_kind_timeintscheme | - Kind of time integration scheme. |
Definition at line 1270 of file config_structure.inl.
|
inline |
Set the value of the non-dimensional thermal conductivity.
Definition at line 904 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 671 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 669 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be plot val_plotting (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_plotting | - 0 or 1 depending if the the marker is going to be plot. |
Definition at line 1343 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be designed val_designing (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_monitoring | - 0 or 1 depending if the the marker is going to be designed. |
Definition at line 1339 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be affected by design variables val_moving (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_DV | - 0 or 1 depending if the the marker is affected by design variables. |
Definition at line 1353 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be monitored val_monitoring (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_monitoring | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 1337 of file config_structure.inl.
|
inline |
Set the value of the boundary val_boundary (read from the config file) for the marker val_marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_boundary | - Kind of boundary read from config file. |
Definition at line 1331 of file config_structure.inl.
|
inline |
Set if a marker val_marker is part of the MixingPlane interface (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_turboperf | - 0 if not part of the MixingPlane interface or greater than 1 if it is part. |
Definition at line 1351 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be monitored val_monitoring (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_monitoring | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 1335 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be moved val_moving (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_moving | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 1355 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be periodic val_perbound (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_perbound | - Index of the surface with the periodic boundary. |
Definition at line 1359 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be plot val_plotting (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_plotting | - 0 or 1 depending if the the marker is going to be plot. |
Definition at line 1341 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be customized in Python val_PyCustom (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_PyCustom | - 0 or 1 depending if the the marker is going to be customized in Python. |
Definition at line 1357 of file config_structure.inl.
|
inline |
Set if a marker val_marker is going to be sent or receive val_index from another domain.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
| [in] | val_index | - Index of the surface read from geometry file. |
Definition at line 1371 of file config_structure.inl.
|
inline |
Set the value of the index val_index (read from the geometry file) for the marker val_marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_index | - Index of the surface read from geometry file. |
Definition at line 1333 of file config_structure.inl.
|
inline |
Set if a marker val_marker is part of the Turbomachinery (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_turboperf | - 0 if not part of Turbomachinery or greater than 1 if it is part. |
Definition at line 1347 of file config_structure.inl.
|
inline |
Set a flag to the marker val_marker part of the Turbomachinery (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_turboperflag | - 0 if is not part of the Turbomachinery, flag INFLOW or OUTFLOW if it is part. |
Definition at line 1349 of file config_structure.inl.
|
inline |
Set if a marker val_marker is part of the FSI interface val_plotting (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_plotting | - 0 or 1 depending if the the marker is part of the FSI interface. |
Definition at line 1345 of file config_structure.inl.
| void CConfig::SetMarkers | ( | unsigned short | val_software | ) |
Config file markers processing.
Definition at line 4059 of file config_structure.cpp.
|
inline |
Set the maximum velocity^2 in the domain for the incompressible preconditioner.
| [in] | Value | of the maximum velocity^2 in the domain for the incompressible preconditioner. |
Definition at line 1943 of file config_structure.inl.
|
inline |
Set the number of multigrid levels.
| [in] | val_nMGLevels | - Index of the mesh were the CFL is applied |
Definition at line 729 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 629 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 631 of file config_structure.inl.
|
inline |
Set Monitor Outlet Pressure value for the ramp.
Definition at line 1200 of file config_structure.inl.
|
inline |
Set x-coordinate of the mesh motion origin.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
| [in] | val_origin | - New x-coordinate of the mesh motion origin. |
Definition at line 918 of file config_structure.inl.
|
inline |
Set y-coordinate of the mesh motion origin.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
| [in] | val_origin | - New y-coordinate of the mesh motion origin. |
Definition at line 920 of file config_structure.inl.
|
inline |
Set z-coordinate of the mesh motion origin.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
| [in] | val_origin | - New y-coordinate of the mesh motion origin. |
Definition at line 922 of file config_structure.inl.
| void CConfig::SetMPICommunicator | ( | SU2_MPI::Comm | Communicator | ) |
Set the MPI communicator for SU2.
| [in] | Communicator | - MPI communicator for SU2. |
Definition at line 158 of file config_structure.cpp.
|
inline |
Set the value of the non-dimensional constant viscosity.
Definition at line 896 of file config_structure.inl.
|
inline |
Set the value of the non-dimensional reference viscosity for Sutherland model.
Definition at line 898 of file config_structure.inl.
|
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Set the value of the non-dimensional S for Sutherland model.
Definition at line 902 of file config_structure.inl.
|
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Set the value of the non-dimensional reference temperature for Sutherland model.
Definition at line 900 of file config_structure.inl.
|
inline |
number Turbomachinery blades computed using the pitch information.
Definition at line 1228 of file config_structure.inl.
|
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Set the number of external iterations.
| [in] | val_niter | - Set the number of external iterations. |
Definition at line 432 of file config_structure.inl.
|
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Set the number of time levels for time accurate local time stepping.
| [in] | val_nLevels | - The number of time levels to be set. |
Definition at line 789 of file config_structure.inl.
|
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Stores the number of marker in the simulation.
| [in] | val_nmarker | - Number of markers of the problem. |
Definition at line 1300 of file config_structure.inl.
|
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Set the current number of non-physical nodes in the solution.
| [in] | val_nonphys_points | - current number of non-physical points. |
Definition at line 1783 of file config_structure.inl.
|
inline |
Set the current number of non-physical reconstructions for 2nd-order upwinding.
| [in] | val_nonphys_reconstr | - current number of non-physical reconstructions for 2nd-order upwinding. |
Definition at line 1787 of file config_structure.inl.
| void CConfig::SetnPeriodicIndex | ( | unsigned short | val_index | ) |
Set the total number of SEND_RECEIVE periodic transformations.
| [in] | val_index | - Total number of transformations. |
Definition at line 7575 of file config_structure.cpp.
|
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set number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 1254 of file config_structure.inl.
|
inline |
set number of maximum span-wise sections among all zones .
Definition at line 1250 of file config_structure.inl.
|
inline |
set number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 1248 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 657 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 653 of file config_structure.inl.
|
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Set the Froude number for free surface problems.
Definition at line 683 of file config_structure.inl.
|
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Set the scale factor for the line search.
| [in] | val_scale | - scale of the deformation. |
Definition at line 1743 of file config_structure.inl.
| void CConfig::SetOutlet_Pressure | ( | su2double | val_pressure, |
| string | val_marker | ||
| ) |
Set the back pressure (static) at an outlet boundary.
| [in] | val_pressure | - Pressure value at the outlet boundary. |
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7698 of file config_structure.cpp.
| void CConfig::SetOutput | ( | unsigned short | val_software, |
| unsigned short | val_izone | ||
| ) |
Config file output.
Definition at line 4658 of file config_structure.cpp.
|
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Set the rotation center for a periodic transformation.
| [in] | val_index | - Index corresponding to the periodic transformation. |
| [in] | center | - Pointer to a vector containing the coordinate of the center. |
Definition at line 1625 of file config_structure.inl.
|
inline |
Set the rotation angles for a periodic transformation.
| [in] | val_index | - Index corresponding to the periodic transformation. |
| [in] | rotation | - Pointer to a vector containing the rotation angles. |
Definition at line 1631 of file config_structure.inl.
|
inline |
Set the translation vector for a periodic transformation.
| [in] | val_index | - Index corresponding to the periodic transformation. |
| [in] | translate | - Pointer to a vector containing the coordinate of the center. |
Definition at line 1637 of file config_structure.inl.
| void CConfig::SetPointersNull | ( | void | ) |
Initializes pointers to null.
Definition at line 359 of file config_structure.cpp.
| void CConfig::SetPostprocessing | ( | unsigned short | val_software, |
| unsigned short | val_izone, | ||
| unsigned short | val_nDim | ||
| ) |
Config file postprocessing.
Definition at line 2467 of file config_structure.cpp.
|
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Set the Froude number for free surface problems.
Definition at line 617 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 615 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 675 of file config_structure.inl.
|
inline |
Set the thermodynamic pressure for low Mach problems.
Definition at line 621 of file config_structure.inl.
|
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Set the non-dimensionalized thermodynamic pressure for low Mach problems.
Definition at line 619 of file config_structure.inl.
| void CConfig::SetPressureOut_BC | ( | su2double | val_press | ) |
Set the outlet pressure imposed as BC for internal flow.
| [in] | val_temp | - New value of the outlet pressure. |
Definition at line 7801 of file config_structure.cpp.
| void CConfig::SetProfilingCSV | ( | void | ) |
Write a CSV file containing the results of the profiling.
Definition at line 8514 of file config_structure.cpp.
|
inline |
In case the RefArea is equal to 0 then, it is necessary to compute a reference area, with this function we set the value of the reference area.
| [in] | val_area | - Value of the reference area for non dimensional coefficient computation. |
Definition at line 426 of file config_structure.inl.
|
inline |
Set reference origin x-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val_origin | - New x-coordinate of the mesh motion origin. |
Definition at line 597 of file config_structure.inl.
|
inline |
Set reference origin y-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val_origin | - New y-coordinate of the mesh motion origin. |
Definition at line 599 of file config_structure.inl.
|
inline |
Set reference origin z-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val_origin | - New z-coordinate of the mesh motion origin. |
Definition at line 601 of file config_structure.inl.
|
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Set the sum of the bandwidth for writing binary restarts (to be averaged later).
| [in] | Sum | of the bandwidth for writing binary restarts. |
Definition at line 1947 of file config_structure.inl.
|
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Set the Froude number for free surface problems.
Definition at line 667 of file config_structure.inl.
|
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Set the angular velocity of the mesh about the z-axis.
| [in] | val_iZone | - Number for the current zone in the mesh (each zone has independent motion). |
| [in] | newRotation_Rate_Z | - new rotation rate after computing the ramp value. |
Definition at line 938 of file config_structure.inl.
| void CConfig::SetRunTime_Options | ( | void | ) |
Set the config options.
Definition at line 635 of file config_structure.cpp.
| bool CConfig::SetRunTime_Parsing | ( | char | case_filename[MAX_STRING_SIZE] | ) |
Set the config file parsing.
Definition at line 2382 of file config_structure.cpp.
|
inline |
In case the SemiSpan is equal to 0 then, it is necessary to compute the max y distance, with this function we set the value of the semi span.
| [in] | val_semispan | - Value of the semispan. |
Definition at line 428 of file config_structure.inl.
|
inline |
Set information about there is a smoothing of the grid coordinates.
| [in] | val_smoothnumgrid | - TRUE if there is smoothing of the grid coordinates; otherwise FALSE. |
Definition at line 1599 of file config_structure.inl.
|
inline |
Set the value of the specific heat at constant pressure (incompressible fluids with energy equation).
| [in] | val_specific_heat_cp | - specific heat at constant pressure. |
Definition at line 691 of file config_structure.inl.
|
inline |
Set the non-dimensional value of the specific heat at constant pressure (incompressible fluids with energy equation).
| [in] | val_specific_heat_cpnd | - non-dim. specific heat at constant pressure. |
Definition at line 639 of file config_structure.inl.
|
inline |
Set the value of the specific heat at constant volume (incompressible fluids with energy equation).
| [in] | val_specific_heat_cv | - specific heat at constant volume. |
Definition at line 693 of file config_structure.inl.
|
inline |
Set the non-dimensional value of the specific heat at constant volume (incompressible fluids with energy equation).
| [in] | val_specific_heat_cvnd | - non-dim. specific heat at constant pressure. |
Definition at line 641 of file config_structure.inl.
| void CConfig::SetSpline | ( | vector< su2double > & | x, |
| vector< su2double > & | y, | ||
| unsigned long | n, | ||
| su2double | yp1, | ||
| su2double | ypn, | ||
| vector< su2double > & | y2 | ||
| ) |
Given arrays x[1..n] and y[1..n] containing a tabulated function, i.e., yi = f(xi), with x1 < x2 < . . . < xN , and given values yp1 and ypn for the first derivative of the interpolating function at points 1 and n, respectively, this routine returns an array y2[1..n] that contains the second derivatives of the interpolating function at the tabulated points xi. If yp1 and/or ypn are equal to 1 × 1030 or larger, the routine is signaled to set the corresponding boundary condition for a natural spline, with zero second derivative on that boundary. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++.
Definition at line 8422 of file config_structure.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 108 of file config_structure.inl.
|
inline |
Set the density at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_density | - Value of the density. |
Definition at line 118 of file config_structure.inl.
|
inline |
Set the enthalpy at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_density | - Value of the density. |
Definition at line 120 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 138 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 140 of file config_structure.inl.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 142 of file config_structure.inl.
|
inline |
Set the mach number at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the mach number. |
Definition at line 112 of file config_structure.inl.
|
inline |
Set the massflow at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the mass flow. |
Definition at line 110 of file config_structure.inl.
|
inline |
Set the momentum distortion at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_momentumdistortion | - Value of the momentum distortion. |
Definition at line 130 of file config_structure.inl.
|
inline |
Set the normal velocity at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_normalvelocity | - Value of the normal velocity. |
Definition at line 122 of file config_structure.inl.
|
inline |
Set the pressure at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the pressure. |
Definition at line 116 of file config_structure.inl.
|
inline |
Set the pressure drop between two surfaces.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_pressuredrop | - Value of the pressure drop. |
Definition at line 136 of file config_structure.inl.
|
inline |
Set the secondary flow strength at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_secondarystrength | - Value of the secondary flow strength. |
Definition at line 126 of file config_structure.inl.
|
inline |
Set the relative secondary flow strength at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_secondaryoverstream | - Value of the relative seondary flow strength. |
Definition at line 128 of file config_structure.inl.
|
inline |
Set the temperature at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the temperature. |
Definition at line 114 of file config_structure.inl.
|
inline |
Set the total pressure at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_totalpressure | - Value of the total pressure. |
Definition at line 134 of file config_structure.inl.
|
inline |
Set the total temperature at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_totaltemperature | - Value of the total temperature. |
Definition at line 132 of file config_structure.inl.
|
inline |
Set the streamwise flow uniformity at the surface.
| [in] | val_imarker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_streamwiseuniformity | - Value of the streamwise flow uniformity. |
Definition at line 124 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 633 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 635 of file config_structure.inl.
|
inline |
Set the reference temperature.
Definition at line 679 of file config_structure.inl.
|
inline |
Set the thermal expansion coefficient.
| [in] | val_thermal_expansion | - thermal expansion coefficient |
Definition at line 695 of file config_structure.inl.
|
inline |
Set the non-dim. thermal expansion coefficient.
| [in] | val_thermal_expansion | - non-dim. thermal expansion coefficient |
Definition at line 643 of file config_structure.inl.
|
inline |
Set the thermal diffusivity for solids.
Definition at line 705 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 681 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 655 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 651 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 663 of file config_structure.inl.
| void CConfig::SetTotalTemperatureIn_BC | ( | su2double | val_temp | ) |
Set the inlet total temperature imposed as BC for internal flow.
| [in] | val_temp | - New value of the total temperature. |
Definition at line 7854 of file config_structure.cpp.
| void CConfig::SetTranspirationParams_DV | ( | ) |
Set the transpiration params using DV values.
| [in] | val_index | - Index corresponding to the transpiration boundary. |
Definition at line 8019 of file config_structure.cpp.
|
inline |
Set the value of the boolean for updating AoA in fixed lift mode.
| [in] | val_update | - the bool for whether to update the AoA. |
Definition at line 1775 of file config_structure.inl.
|
inline |
Set the value of the boolean for updating AoA in fixed lift mode.
| [in] | val_update | - the bool for whether to update the AoA. |
Definition at line 1779 of file config_structure.inl.
|
inline |
Set the free-stream velocity.
| [in] | val_velocity_freestream | - Value of the free-stream velocity component. |
| [in] | val_dim | - Value of the current dimension. |
Definition at line 645 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 647 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 673 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 627 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 649 of file config_structure.inl.
|
inline |
Set the Froude number for free surface problems.
Definition at line 699 of file config_structure.inl.
|
inline |
Set the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.
Definition at line 1278 of file config_structure.inl.
|
inline |
Set the frequency for writing the convergence file.
Definition at line 840 of file config_structure.inl.
|
inline |
Set information about writing a template inlet profile file.
| [in] | val_wrt_inletfile | - flag for whether to write a template inlet profile file. |
Definition at line 1673 of file config_structure.inl.
|
inline |
Subtract one to the index of the finest grid (full multigrid strategy).
Definition at line 735 of file config_structure.inl.
| void CConfig::Tick | ( | double * | val_start_time | ) |
Start the timer for profiling subroutines.
| [in] | val_start_time | - the value of the start time. |
Definition at line 8477 of file config_structure.cpp.
| void CConfig::Tock | ( | double | val_start_time, |
| string | val_function_name, | ||
| int | val_group_id | ||
| ) |
Stop the timer for profiling subroutines and store results.
| [in] | val_start_time | - the value of the start time. |
| [in] | val_function_name | - string for the name of the profiled subroutine. |
| [in] | val_group_id | - string for the name of the profiled subroutine. |
Definition at line 8490 of file config_structure.cpp.
| bool CConfig::TokenizeString | ( | string & | str, |
| string & | option_name, | ||
| vector< string > & | option_value | ||
| ) |
breaks an input line from the config file into a set of tokens
| [in] | str | - the input line string |
| [out] | option_name | - the name of the option found at the beginning of the line |
| [out] | option_value | - the tokens found after the "=" sign on the line |
Definition at line 6307 of file config_structure.cpp.
| vector<string> CConfig::fields |
Tags for the different fields in a restart file.
Definition at line 1369 of file config_structure.hpp.
1.9.1